|
||||||||||
| PREV NEXT | FRAMES NO FRAMES | |||||||||
BigFraction.
AbsoluteDate.J2000_EPOCH).
time scale.
time scale.
time scale.
time scale.
time scale.
time scale.
time scale.
time scale.
time scale.
time scale.
AbsoluteDateInterval.AbsoluteDateInterval instances ; as the
AbsoluteDateInterval objects implement the ComparableInterval
class, the list is an ordered collection of time intervals.AttitudeLegsSequence.AttitudeLaw interface.CelestialBody interface.AbstractUnivariateDifferentiableSolverFieldMatrix methods regardless of the underlying storage.FractionFormat and BigFractionFormat.AbstractIntegerDistribution.AbstractIntegerDistribution(RandomGenerator) instead.
SimpleValueChecker.SimpleValueChecker()
MSISE2000 atmosphere model.Propagator methods for analytical propagators.RandomGenerator interface.AbstractRealDistribution.AbstractRealDistribution(RandomGenerator) instead.
SimpleValueChecker.SimpleValueChecker()
Slew interface.StelaGTOPropagator.StorelessUnivariateStatistic interface.SubHyperplane.ForceModel methods for tides models.Parameter.
Parameter.
UnivariateStatistic interface.Adams-Bashforth and
Adams-Moulton integrators.EventDetector to commons-math
EventHandler interface.AdaptedEventDetector and adapted to multi
propagation.AdaptedEventDetector and adapted to multi
propagation.OrekitStepHandler
to commons-math StepHandler interface.differential effects.CodedEvent to the list.
Phenomenon to the list.
DateDetector, always add the
maneuver;
the maneuver to add is triggered by a DateDetector, check if the date of the maneuver
respects the two following conditions:
no superposition with any maneuver in the list;
the time between the end of the previous maneuver and the date of the maneuver to add, as well as the time
between the end of the maneuver to add and the date of the next maneuver, must be bigger than the threshold
value.
FunctionUtils.add(UnivariateDifferentiableFunction...)
TrigonometricPolynomialFunction
TrigonometricPolynomialPrimitive
PolynomialFunction
TrigonometricPolynomialFunction
Complex whose value is
(this + addend).
Complex whose value is (this + addend),
with addend interpreted as a real number.
BigInteger,
returning the result in reduced form.
this and m.
m to this matrix.
this and m.
this and v.
this and v.
v.
this and m.
this and m.
m.
this and m.
this and m.
this and v.
m.
v.
this and m.
v.
this and v.
m.
m.
this and m.
OceanTidesCoefficientsSet to the data map
GeoMagneticField to the models list.
Collection of chromosomes to this Population.
data.
SpacecraftState.ResizableDoubleArray.ExpansionMode.ADDITIVE instead.
Orbit.orbitAddKeplerContribution(PositionAngle, double, double[])
implemented in inherited classes of Orbit.
this matrix.
this matrix.
this matrix.
this matrix.
this matrix.
this matrix.
this matrix.
Parameter.
Parameter
Parameter without the atmospheric height scale.
DragWrenchSensitive assembly model.SummaryStatistics from several data sets or
data set partitions.(bracketed univariate real) root-finding algorithm may accept as solutions.AbstractPropagator class.Vector3D.ZERO).
TimeStampedAngularCoordinates
interpolation.double[]
arrays.
double[]
arrays.
spacecraft state.
spacecraft state.
Math.FieldElement[][] array to store entries.FieldMatrix<T> with the supplied row and column dimensions.
FieldMatrix<T> using the input array as the underlying
data array.
FieldMatrix<T> using the input array as the underlying
data array.
FieldMatrix<T> using the input array as the underlying
data array.
FieldMatrix<T> using the input array as the underlying
data array.
FieldMatrix<T> using v as the
data for the unique column of the created matrix.
FieldMatrix<T> using v as the
data for the unique column of the created matrix.
RealMatrix using a double[][] array to
store entries.RealMatrix using the input array as the underlying
data array.
v as the
data for the unique column of the created matrix.
FieldVector interface with a FieldElement array.RealVector interface with a double array.Assert.assertEquals(double, double, double) method.
Assert.assertEquals(double, double, double) method
for a relative comparison.
Frame class; it represents a dynamic spacecraft frame,
i.e.AttitudeLeg.TransformProvider for AttitudeFrame; it provides, for a given date,
the transformation corresponding to the spacecraft reference frame orientation with respect to the parent frame.GroundMaskElevationDetector detector.SimpleValueChecker.SimpleValueChecker()
SimpleValueChecker.SimpleValueChecker()
SimpleVectorValueChecker.SimpleVectorValueChecker()
OrekitStepInterpolator interface based
on a Propagator.BigDecimal.
BigDecimal following the passed
rounding mode.
BigDecimal following the passed scale
and rounding mode.
BigFraction equivalent to the passed BigInteger, ie
"num / 1".
BigFraction given the numerator and denominator as
BigInteger.
BigFraction equivalent to the passed int, ie
"num / 1".
BigFraction given the numerator and denominator as simple
int.
BigFraction equivalent to the passed long, ie "num / 1".
BigFraction given the numerator and denominator as simple
long.
FieldMatrix/BigFraction matrix to a RealMatrix.
BinaryChromosomes.n choose k", the number of
k-element subsets that can be selected from an
n-element set.
n choose k", the number of
k-element subsets that can be selected from an
n-element set.
double representation of the Binomial
Coefficient, "n choose k", the number of
k-element subsets that can be selected from an
n-element set.
double representation of the Binomial
Coefficient, "n choose k", the number of
k-element subsets that can be selected from an
n-element set.
log of the Binomial
Coefficient, "n choose k", the number of
k-element subsets that can be selected from an
n-element set.
log of the Binomial
Coefficient, "n choose k", the number of
k-element subsets that can be selected from an
n-element set.
BodyCenterPointing and
this class is that the target point of the former is the body center, while that of the latter is the corresponding
point on the ground. lowerBound <= a < initial < b <= upperBound
f(a) * f(b) < 0
If f is continuous on [a,b], this means that a
and b bracket a root of f.
lowerBound <= a < initial < b <= upperBound
f(a) * f(b) <= 0
If f is continuous on [a,b], this means that a
and b bracket a root of f.
(univariate real) root-finding
algorithms that maintain a bracketed solution.100, 50 (see the
other constructor).
100, 50 (see the
other constructor).
(lo, hi), this class
finds an approximation x to the point at which the function
attains its minimum.BSP tree nodes.CodedEvent instance appropriate for the provided SpacecraftState.
CodedEvent instance appropriate for the provided map of SpacecraftState.
CodedEventsList, one list per CodingEventDetector instance.
CodedEventsList, one list per MultiCodingEventDetector instance.
CodedEvent instance appropriate for the provided SpacecraftState.
CodedEvent instance appropriate for the provided map of SpacecraftState.
CodedEvent instance appropriate for the provided SpacecraftState.
CodedEvent instance appropriate for the provided map of SpacecraftState.
PhenomenaList, one list per CodingEventDetector instance.
PhenomenaList, one list per MultiCodingEventDetector instance.
byte.
WeibullDistribution.getNumericalMean()
ZipfDistribution.getNumericalMean().
FDistribution.getNumericalVariance()
HypergeometricDistribution.getNumericalVariance().
WeibullDistribution.getNumericalVariance()
ZipfDistribution.getNumericalVariance().
TimeStampedPVCoordinates and
interpolation.P(D_n < d) using method described in [1] with quick
decisions for extreme values given in [2] (see above).
P(D_n < d) using method described in [1] with quick
decisions for extreme values given in [2] (see above).
P(D_n < d) using method described in [1] with quick
decisions for extreme values given in [2] (see above).
ceil function.ResizableDoubleArray.checkContractExpand(double,double) instead.
solve and
solveInPlace,
and throws an exception if one of the checks fails.
solve
and
solveInPlace,
and throws an exception if one of the checks fails.
PolygonsSet.PolygonsSet(Vector2D[][]) is used,
second exception cannot be reached (vertices are automatically sorted in TRIGO sense, which prevent crossing borders)
If constructor PolygonsSet.PolygonsSet(Vector2D[][]) is used,
third exception cannot be reached (the first will be reached before)
representation can represent a valid chromosome.
representation can represent a valid chromosome.
representation can represent a valid chromosome.
observed and expected
frequency counts.
counts
array, viewed as a two-way table.
observed1 and observed2.
observed
frequency counts to those in the expected array.
alpha.
counts
array, viewed as a two-way table.
alpha.
observed1 and
observed2.
Chromosome objects.TimeStamped instance.CIPCoordinates to be used independently or within a
TimeStampedCache.CircularOrbit.CircularOrbit(double, double, double,
double, double, double, PositionAngle, Frame, AbsoluteDate, double)
MSISE2000 atmosphere model
This model of input parameters computes averages for SOME of the ap values required by the MSISE2000 model.AbstractRandomGenerator.nextGaussian().
BitsStreamGenerator.nextGaussian.
valuesFileURL after use in REPLAY_MODE.
Clusterable points.lambda must be
passed with the call to optimize (whereas in the current code it is set to an undocumented value).
lambda must be
passed with the call to optimize (whereas in the current code it is set to an undocumented value)..
lambda and inputSigma must be
passed with the call to optimize.
SimpleValueChecker.SimpleValueChecker()
lambda and inputSigma must be
passed with the call to optimize.
CodedEvent.CodingEventDetector is used, via the
monitorDetector method.CodedEvent object.(n, k) of k elements in a set of
n elements.int[] arrays.
h(x) = combiner(f(x), g(x)).
a * this + b * y, the linear
combination of this and y.
a * this + b * y, the linear
combination of this and y.
this with the linear combination of this and
y.
this with the linear combination of this and
y.
Comparable data.MathIllegalArgumentException is thrown.
data sorted by comparator.
CodedEvent instances.CodedEvent is consistent with equals,
so that a CodedEvent can be used in any SortedSet or SortedMap.new Double(this.doubleValue()).compareTo(new
Double(o.doubleValue()))
Complex utilities functions.UnivariateFunction cos(intermediateOrder * omega * x) or sin
FunctionUtils.compose(UnivariateDifferentiableFunction...)
BalminoAttractionModel).
valuesFileURL, using the default number of bins.
valuesFileURL and binCount bins.
DrozinerAttractionModel).
EcksteinHechlerPropagator.osc2mean(Orbit) instead
p1, at a distance d,
in a direction defined from an azimuth.
n-th roots of unity.
OrientationFunction using the quaternions formula:
Ω = 2 * Q' dQ, where Q' is the conjugate of the quaternion and dQ is the derivative of the quaternion at
the given date.
Vector3DFunction from the current OrientationFunction using the quaternions formula:
Ω = 2 * Q' dQ, where Q' is the conjugate of the quaternion and dQ is the derivative of the quaternion at
the given date.
RealLinearOperator.Parameter.
Parameter.
Parameter.
Parameter with a local orbital frame defined by its type.
MSISE2000 atmosphere model
This model of input parameters computes averages for ALL the ap values required by the MSISE2000 model.Complex objects.
source array.
source array.
source array.
source array.
RandomVectorGenerator that generates vectors with with
correlated components.AbstractLeastSquaresOptimizer.setCost(double).
Random using the supplied
RandomGenerator.
FieldMatrix using the data from the input
array.
RealMatrix using the data from the input
array.
Complex from the specified two dimensional
array of real and imaginary parts.
SummaryStatistics whose data will be
aggregated with those of this AggregateSummaryStatistics.
dimension x dimension identity matrix.
FieldMatrix with specified dimensions.
FieldMatrix whose entries are the the values in the
the input array.
FieldVector using the data from the input array.
IllegalArgumentException with localized message.
IllegalStateException with localized message.
RuntimeException for an internal error.
ParseException with localized message.
dimension x dimension identity matrix.
double filled with the real
and imaginary parts of the specified Complex numbers.
RealMatrix with specified dimensions.
RealMatrix whose entries are the the values in the
the input array.
RealVector using the data from the input array.
FieldMatrix using the data from the input
array.
RealMatrix using the data from the input
array.
X whose values are distributed according
to this distribution, this method returns P(x0 < X <= x1).
AbstractRealDistribution.probability(double,double) instead.
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(x0 < X <= x1).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
RealDistribution.cumulativeProbability(double,double)
X whose values are distributed according
to this distribution, this method returns P(X <= x).
RealDistribution.cumulativeProbability(double,double)
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
probability(double x0, double x1).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
X whose values are distributed according
to this distribution, this method returns P(X <= x).
Parameter.
Parameter.
CurveFitter.CurveFitter(MultivariateDifferentiableVectorOptimizer)
CycleCrossover policy.
CycleCrossover policy using the given randomStart behavior.
data providers.file loaders.data providers.DateComponents.J2000_EPOCH.
double value in an object.sequence of objects of type T according to the
permutation this chromosome represents.
sequence of objects of type T according to the
permutation this chromosome represents.
f, using user given period t and integrator, into a
Fourier Series of order order.
CMAESOptimizer.checkFeasableCount: 0.
CMAESOptimizer.diagonalOnly: 0.
RealMatrix objects.
BOBYQAOptimizer.initialTrustRegionRadius: 10.0 .
BOBYQAOptimizer.initialTrustRegionRadius: 10.0 .
CMAESOptimizer.isActiveCMA: true.
CMAESOptimizer.maxIterations: 30000.
CMAESOptimizer.random.
CMAESOptimizer.stopFitness: 0.0.
BOBYQAOptimizer.stoppingTrustRegionRadius: 1.0E-8 .
BOBYQAOptimizer.stoppingTrustRegionRadius: 1.0E-8 .
FieldMatrixChangingVisitor interface.FieldMatrixPreservingVisitor interface.IterativeLinearSolverEvent.MeasurementModel for the use with a KalmanFilter.MeasurementModel, taking double arrays as input parameters for the
respective measurement matrix and noise.
MeasurementModel, taking RealMatrix objects
as input parameters for the respective measurement matrix and noise.
ProcessModel for the use with a KalmanFilter.ProcessModel, taking double arrays as input parameters.
ProcessModel, taking double arrays as input parameters.
ProcessModel, taking double arrays as input parameters.
RealMatrixChangingVisitor interface.RealMatrixPreservingVisitor interface.x.
x.
x.
x.
x.
x.
x.
x.
x.
x.
x.
x.
x.
x.
x.
x.
x.
Acos.value(DerivativeStructure)
Acosh.value(DerivativeStructure)
Asin.value(DerivativeStructure)
Asinh.value(DerivativeStructure)
Atan.value(DerivativeStructure)
Atanh.value(DerivativeStructure)
Cbrt.value(DerivativeStructure)
Constant.value(DerivativeStructure)
Cos.value(DerivativeStructure)
Cosh.value(DerivativeStructure)
Exp.value(DerivativeStructure)
Expm1.value(DerivativeStructure)
Gaussian.value(DerivativeStructure)
HarmonicOscillator.value(DerivativeStructure)
Identity.value(DerivativeStructure)
Inverse.value(DerivativeStructure)
Log.value(DerivativeStructure)
Log10.value(DerivativeStructure)
Log1p.value(DerivativeStructure)
Logistic.value(DerivativeStructure)
Logit.value(DerivativeStructure)
Minus.value(DerivativeStructure)
Power.value(DerivativeStructure)
Sigmoid.value(DerivativeStructure)
Sin.value(DerivativeStructure)
Sinc.value(DerivativeStructure)
Sinh.value(DerivativeStructure)
Sqrt.value(DerivativeStructure)
Tan.value(DerivativeStructure)
Tanh.value(DerivativeStructure)
UnivariateFunction.
OrientationFunction representing the first derivative of the current orientation function
components.OrientationFunction representing the first derivative of the current orientation function
components.RealMatrix field in a class.
RealVector field in a class.
Dfp which hides the radix-10000 artifacts of the superclass.Dfp.UnivariateFunction representing a differentiable and integrable univariate real function.MultivariateDifferentiableFunctionMultivariateDifferentiableVectorFunctionUnivariateDifferentiableFunctionUnivariateDifferentiableMatrixFunctionUnivariateDifferentiableSolverUnivariateDifferentiableVectorFunctiondifferential from a regular function.
differential from a regular vector function.
differential from a regular matrix function.
UnivariateFunction on a single point using the Ridders method.
differential from a regular function.
differential from a regular function.
differential from a regular matrix function.
differential from a regular vector function.
i initial elements of the array.
i last elements of the array.
Complex whose value is
(this / divisor).
Complex whose value is (this / divisor),
with divisor interpreted as a real number.
BigInteger,
ie this * 1 / bg, returning the result in reduced form.
int, ie
this * 1 / i, returning the result in reduced form.
long, ie
this * 1 / l, returning the result in reduced form.
v.
v.
Parameter.
Parameter.
DTM2000 atmosphere modelLocalizable interface, without localization.RealVector might lead to wrong results. Since there is no
satisfactory correction to this bug, this method is deprecated. Users who
want to preserve this feature are advised to implement
RealVectorPreservingVisitor (possibly ignoring corner cases for
the sake of efficiency).
RealVector might lead to wrong results. Since there is no
satisfactory correction to this bug, this method is deprecated. Users who
want to preserve this feature are advised to implement
RealVectorPreservingVisitor (possibly ignoring corner cases for
the sake of efficiency).
PositionAngle
PositionAngle
PositionAngle
SpacecraftState
using the analytical Eckstein-Hechler model.TrigonometricPolynomialFunction by an ElementaryMultiplicationTypes
ElitisticListPopulation instance.
ElitisticListPopulation instance and initializes its inner chromosome list.
RandomGenerator as the source of random data.
RandomGenerator as the source of random data.
EmpiricalDistribution.EmpiricalDistribution(int,RandomGenerator) instead.
EmpiricalDistribution.EmpiricalDistribution(RandomGenerator) instead.
Parameter for A; B and C coef
with a given LOF frame.
Parameter for A; B and C coef
with a given frame.
TransformProvider for FramesFactory.getEODFrame(boolean).AbstractBoundedPVProvider
which implements PVCoordinatesProvider
and so provides a position velocity for a given date.AbstractBoundedPVProvider
which implements PVCoordinatesProvider
and so provides a position velocity for a given date.1 + EPSILON is numerically equal to 1.
CodedEvent as another
instance.
Phenomenon as another instance.
object is a
FieldMatrix instance with the same dimensions as this
and all corresponding matrix entries are equal.
object is a
RealMatrix instance with the same dimensions as this
and all corresponding matrix entries are equal.
object is an
AbstractStorelessUnivariateStatistic returning the same
values as this for getResult() and getN()
object is a MultivariateSummaryStatistics
instance and all statistics have the same values as this.
object is a
StatisticalSummaryValues instance and all statistics have
the same values as this.
object is a
SummaryStatistics instance and all statistics have the
same values as this.
object is a MultivariateSummaryStatistics
instance and all statistics have the same values as this.
object is a
SummaryStatistics instance and all statistics have the
same values as this.
Precision.equals(float,float).
true iff both arguments are null or have same
dimensions and all their elements are equal as defined by
Precision.equals(double,double).
equals(x, y, 1).
equals(x, y, 1).
true if there is no double value strictly between the
arguments or the difference between them is within the range of allowed
error (inclusive).
ComparableInterval as another instance.
this method.
true iff both arguments are null or have same
dimensions and all their elements are equal as defined by
this method.
equals(x, y, 1).
equals(x, y, maxUlps).
equals(x, y, 1).
equals(x, y, maxUlps).
Precision.equalsWithRelativeTolerance(double, double, double).
true if there is no double value strictly between the
arguments or the reltaive difference between them is smaller or equal
to the given tolerance.
true if both arguments are found equal
with a relative comparison using a default epsilon.
EquinoctialOrbit.EquinoctialOrbit(double, double, double,
double, double, double, PositionAngle, Frame, AbsoluteDate, double)
OrientationFunction using the
AngularCoordinates.estimateRate(Rotation, Rotation, double) method.
Vector3DFunction from the current OrientationFunction using the
AngularCoordinates.estimateRate(Rotation, Rotation, double) method.
Vector3DFunction from the current OrientationFunction using the
AngularCoordinates.estimateRate(Rotation, Rotation, double) method.
AngularCoordinates.estimateRate(Rotation, Rotation, double)
Clusterable for points with double coordinates.Clusterable for points with integer coordinates.P(x) = a0 + a(k) * cos(kx) + b(k) * sin(kx)
P(x) = a0 + a(k) * cos(kx) + b(k) * sin(kx)
AbstractStorelessUnivariateStatistic.clear(), then invokes
AbstractStorelessUnivariateStatistic.increment(double) in a loop over the the input array, and then uses
AbstractStorelessUnivariateStatistic.getResult() to compute the return value.
AbstractStorelessUnivariateStatistic.clear(), then invokes
AbstractStorelessUnivariateStatistic.increment(double) in a loop over the specified portion of the input
array, and then uses AbstractStorelessUnivariateStatistic.getResult() to compute the return value.
Double.NaN if the designated subarray
is empty.
Double.NaN if the designated subarray
is empty.
SemiVariance of the designated values against the mean, using
instance properties varianceDirection and biasCorrection.
SemiVariance for the entire array against the mean, using
the current value of the biasCorrection instance property.
SemiVariance of the designated values against the cutoff, using
instance properties variancDirection and biasCorrection.
SemiVariance of the designated values against the cutoff in the
given direction, using the current value of the biasCorrection instance property.
SemiVariance of the designated values against the cutoff
in the given direction with the provided bias correction.
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
Double.NaN if the designated subarray
is empty.
Double.NaN if the designated subarray
is empty.
Double.NaN if the designated subarray
is empty.
quantileth percentile of the
values array.
pth percentile of the values
in the values array.
quantileth percentile of the
designated values in the values array.
pth percentile of the values
in the values array, starting with the element in (0-based)
position begin in the array and including length
values.
Double.NaN if the designated subarray
is empty.
Double.NaN if the designated subarray
is empty.
Double.NaN if the designated subarray
is empty.
Double.NaN if the designated subarray
is empty.
event handler during integration steps.event detector during integration steps.int.
ExceptionContext interface.ex-1 function.SolarActivityDataProvider
A averaged duration d
It is built with the following convention:
It returns solar activity from user-provided solar activity data provider if date is within timespan of the
user-provided solar activity data provider.
It returns an average of first available solar data over user-defined period d if date is before
lower boundary of the user-provided solar activity data provider.
It returns an average of last available solar data over user-defined period d if date is after
upper boundary of the user-provided solar activity data provider.
ExtremaElevationDetector.MIN, ExtremaElevationDetector.MAX
and ExtremaElevationDetector.MIN_MAX for both.n (the product of the numbers 1 to n), as a
double.
n (the product of the numbers 1 to n), as a
double.
n.
n.
FramesFactory.Math and
StrictMath for large scale computation.Rotation using RealFieldElement.Vector3D using RealFieldElement.length with values generated
using getNext() repeatedly.
InputStream, bypassing the Orekit data loaders.
InputStream, bypassing the Orekit data loaders.
InputStream, bypassing the Orekit data loaders.
InputStream, bypassing the Orekit data loaders.
EOP1980History instance from a collection of EOP1980Entry.
EOP2000History instance from a collection of EOP2000Entry.
population for another chromosome with the same representation.
PolynomialFitter.fit(double[]) instead.
states.
states.
states.
DataProvidersManager.FixedDelayModel instance.
FixedDelayModel instance, and loads the
delay values from the given resource via the DataProvidersManager.
FixedElapsedTime instance.
FixedElapsedTime instance.
AttitudeLegsSequence,
using a fixed time step.float.
floor function.ComplexFormat.format(Object,StringBuffer,FieldPosition).
ComplexFormat.format(Object,StringBuffer,FieldPosition).
Complex object to produce a string.
BigFraction object to produce a string.
Fraction object to produce a string.
BigFraction object to produce a string.
Fraction object to produce a string.
Vector object to produce a string.
Vector3D object to produce a string.
Vector object to produce a string.
Vector object to produce a string.
Vector object to produce a string.
Vector to produce a string.
RealMatrixFormat.format(RealMatrix,StringBuffer,FieldPosition).
RealMatrix object to produce a string.
RealVectorFormat.format(RealVector,StringBuffer,FieldPosition).
RealVector object to produce a string.
UnivariateFunction as a Fourier Series using TrigonometricPolynomialFunction
representation.FourierSeries.
UnivariateFunction and its FourierSeries approximationFieldMatrix/Fraction matrix to a RealMatrix.
UpdatableFrame.updateTransform(Frame, Frame, Transform, AbsoluteDate) method.FramesConfiguration.observed and expected
frequency counts.
Gaussian function.norm, mean, and sigma
of a Gaussian.Parametric
based on the specified observed points.norm, mean, and sigma
of a Gaussian.Parametric
based on the specified observed points.integrating a weighted
function.points and weights.
Gaussian integration rule.SimpleVectorValueChecker.SimpleVectorValueChecker()
SimpleVectorValueChecker.SimpleVectorValueChecker()
observed1 and observed2.
CodingEventDetector interface.EventDetector provided in the constructor.GenericCodingEventDetector that supports a Phenomenon.GenericCodingEventDetector that supports a Phenomenon.GenericCodingEventDetector that does not
support a Phenomenon.
GenericCodingEventDetector that does not
support a Phenomenon.MathIllegalArgumentException is thrown.
GeoMagneticField models.GeometricMean identical
to the original
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
assemblies.alpha.
GammaDistribution.getShape() should be preferred.
This method will be removed in version 4.0.
AttitudeLeg corresponding to the date.
beta.
GammaDistribution.getScale() should be preferred.
This method will be removed in version 4.0.
SummaryStatistics instances containing
statistics describing the values in each of the bins.
true if positive-definiteness should be checked for both
matrix and preconditioner.
true if symmetry of the matrix, and symmetry as well as
positive definiteness of the preconditioner should be checked.
CodedEventsList.
CodedEventsList.
col as an array.
col as an array.
col as an array.
column
as a column matrix.
column
as a column matrix.
column
as a column matrix.
column
as a vector.
column
as a vector.
column
as a vector.
ResizableDoubleArray.getContractionCriterion()
instead.
getCorrelationStandardErrors().getEntry(i,j) is the standard
error associated with getCorrelationMatrix.getEntry(i,j)
AbstractLeastSquaresOptimizer.computeCovariances(double[],double)
instead.
AbstractLeastSquaresOptimizer.computeCovariances(double[],double)
instead.
CrossoverPolicy.
Data object.
FieldVector.toArray() method instead.
SparseFieldVector.toArray() method instead.
BigInteger.
CodingEventDetector that generated the coded event.
AbsoluteDate.durationFrom().DoubleArray.
ResizableArray.
EmpiricalDistribution used when operating in 0.
DateDetector as been provided).
DateDetector as been provided).
DateDetector as been provided).
AbsoluteDate.AbsoluteDate(long, double) constructor.
CodedEvent following some criteria.detectors that have been added.
ResizableDoubleArray.ExpansionMode in 4.0.
BracketFinder.getHi().
BracketFinder.getHi().
Field to which the instance belongs.
Field to which the instance belongs.
Field (really a DfpField) to which the instance belongs.
Field to which the instance belongs.
Field to which the instance belongs.
Field to which the instance belongs.
Field to which the instance belongs.
Field to which the instance belongs.
GeoMagneticField for the given model type and year.
GeoMagneticField for the given model type and year.
BracketFinder.getLo().
BracketFinder.getLo().
BracketFinder.getMid().
BracketFinder.getMid().
CelestialBody.getInertiallyOrientedFrame()
StoppingCondition in the last run.
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
GroundPointingWrapper.getUnderlyingAttitudeLaw()
k-th n-th root of unity.
ISearchIndex.SearchIndexIntervalConvention.CLOSED_OPEN.
ISearchIndex.SearchIndexIntervalConvention.CLOSED_OPEN.
ISearchIndex.SearchIndexIntervalConvention.OPEN_CLOSED.
ISearchIndex.SearchIndexIntervalConvention.OPEN_CLOSED.
SimpleRegression.hasIntercept() is true; otherwise 0.
AbsoluteDateIntervalsList containing the specified date.
this event
is created.
Transform.transformPVCoordinates(PVCoordinates) method of the transform.
Interval.getSize()
Phenomenon.
CodedEventsLogger.LoggedCodedEvent, sorted by date.
MultiCodedEventsLogger.MultiLoggedCodedEvent, sorted by date.
Interval.getInf()
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
Interval.getBarycenter()
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
c of this distribution.
Collection of GeoMagneticField models.
Collection of the GeoMagneticField models that
have been successfully loaded.
ValueServer.GAUSSIAN_MODE, ValueServer.EXPONENTIAL_MODE
or ValueServer.UNIFORM_MODE.
MultiCodingEventDetector that generated the coded event.
Covariance method is not supported by a StorelessCovariance,
since the number of bivariate observations does not have to be the same for different
pairs of covariates - i.e., N as defined in Covariance.getN() is undefined.
TimeStampedCache.getNeighbors(AbsoluteDate).
AttitudeLeg law.
AttitudeLeg law with the selected code.
SpinStabilized.getUnderlyingAttitudeLaw()
BigInteger.
AbsoluteDate.AbsoluteDate(long, double) constructor.
optimize.
optimize.
optimize.
optimize.
optimize.
optimize.
optimize.
SP3File.SP3OrbitType for this SP3 file.
parameter.
parameter.
Phenomenon following some criteria.Phenomenon, provides a code for
the phenomenon associated to the event.
Phenomenon, provides a code for
the phenomenon associated to the event.
index.
index.
AttitudeLeg law.
AttitudeLeg law.
PVCoordinates of the sensor part in the selected frame.
PVCoordinates of the station antenna in the selected frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the spacecraft frame origin in the selected frame.
PVCoordinates of the topocentric frame origin in the selected frame.
PVCoordinates in a specified frame.
PVCoordinates of the body in the selected frame.
PVCoordinates in definition frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the body in the selected frame.
PVCoordinates in orbit definition frame.
PVCoordinates in given output frame.
PVCoordinates of the body in the selected frame.
PVCoordinates of the body in the selected frame.
Dfp instances built by this factory.
PearsonsCorrelation instance constructed from the
ranked input data.
CrossoverPolicy.
k-th n-th root of unity.
BigFraction instance with the 2 parts of a fraction
Y/Z.
Fraction instance with the 2 parts
of a fraction Y/Z.
RoundingMode.HALF_UP
row as an array.
row as an array.
row as an array.
row
as a row matrix.
row
as a row matrix.
row
as a row matrix.
row
as a vector.
row as a vector.
row
as a vector.
row as a vector.
row
as a vector.
row as a vector.
StatisticalSummary describing this distribution.
Collection of SatelliteInformation objects for
all satellites contained in this orbit file.
Collection of SatelliteInformation objects for
all satellites contained in this orbit file.
this distribution.
beta.
this distribution.
alpha.
ValueServer.GAUSSIAN_MODE.
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
DateDetector as been provided).
DateDetector as been provided).
DateDetector as been provided).
SpacecraftState that caused the coded event.
SpacecraftState that caused the coded event.
BufferedReader from a File object.
BufferedReader from a url to a text file.
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
StatisticalSummaryValues instance reporting current
aggregate statistics.
StatisticalSummaryValues instance reporting current
statistics.
StatisticalSummaryValues instance reporting current
statistics.
MultivariateSummaryStatistics.addValue(double[])
MultivariateSummaryStatistics.addValue(double[])
OrbitFile.TimeSystem used to time-stamp position entries.
OrbitFile.TimeSystem used to time-stamp position entries.
Transform embedding an affine transform.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
Transform corresponding to specified date.
SP3File.SP3FileType associated with this SP3 file.
Interval.getSup()
ValueServer.DIGEST_MODE.
BisectionSolver.BisectionSolver(double, double)).
x.
x.
x.
x.
x.
observed frequency counts to those in the expected array.
alpha.
observed1 and
observed2.
AbstractLeastSquaresOptimizer.computeSigma(double[],double) should be used
instead. It should be emphasized that guessParametersErrors and
computeSigma are not strictly equivalent.
new Double(this.doubleValue()).hashCode()
Helmert transformations.StatisticalSummary instances, under the
assumption of equal subpopulation variances.
sample1
and sample2 are drawn from populations with the same mean,
with significance level alpha, assuming that the
subpopulation variances are equal.
this and y
- sqrt(this2 +y2)x and y
- sqrt(x2 +y2)this and y
- sqrt(this2 +y2)x and y
- sqrt(x2 +y2)X = Lon
Y = LatRealLinearOperator is too high.Variance.increment(double) should increment
the internal second moment.
AbstractStorelessUnivariateStatistic.increment(double) in a loop over
the input array.
AbstractStorelessUnivariateStatistic.increment(double) in a loop over
the specified portion of the input array.
MaxCountExceededException.permutedData when applied to
originalData.
UpdatableFrame as an input argument.
SpacecraftState as an input argument.
UnivariateFunction representing an integrable univariate real function.f(x) * w(x),
where w is a weight function that depends on the actual
flavor of the Gauss integration scheme.
SplineInterpolator
on the resulting fit.
TimeStampedAngularCoordinates.interpolate(AbsoluteDate, AngularDerivativesFilter, Collection)
TimeStampedAngularCoordinates.interpolate(AbsoluteDate, AngularDerivativesFilter, Collection, boolean)
TimeStampedPVCoordinates.interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection)
int.
true if RootsOfUnity.computeRoots(int) was called with a
positive value of its argument n.
Rotation.distance(Rotation, Rotation)
Double.POSITIVE_INFINITY or
Double.NEGATIVE_INFINITY) and neither part
is NaN.
NaN.
NaN.
NaN.
true if this double precision number is infinite
(Double.POSITIVE_INFINITY or Double.NEGATIVE_INFINITY).
NaN.
NaN.
NaN.
NaN.
true if this double precision number is
Not-a-Number (NaN), false otherwise.
Frame.isPseudoInertial()
true iff another has the same representation and therefore the same fitness.
true iff another is a RandomKey and
encodes the same permutation.
DataProvidersManager.isSupported(DataProvider)
true if this operator supports
RealLinearOperator.operateTranspose(RealVector).
IterationManager should be derived.IterativeLinearSolver.T1 T2 T3 D R1 R2 R3mm mm mm 10-9 mas mas mas0.1 -0.8 -5.8 0.40 0.000 0.000 0.000+/- 0.3 0.3 0.3 0.05 0.012 0.012 0.012Rates -0.2 0.1 -1.8 0.08 0.000 0.000 0.000+/- 0.3 0.3 0.3 0.05 0.012 0.012 0.012T1 T2 T3 D R1 R2 R3mm mm mm 10-9 mas mas mas-0.5 -0.9 -4.7 0.94 0.000 0.000 0.000+/- 0.2 0.2 0.2 0.03 0.008 0.008 0.008Rates 0.3 0.0 0.0 0.00 0.000 0.000 0.000+/- 0.2 0.2 0.2 0.03 0.008 0.008 0.008secondary equations to
compute the Jacobian matrices with respect to the initial state vector and, if
any, to some parameters of the primary ODE set.IJacobiansParameterizable.java.util.Random to implement
RandomGenerator.Constants.JULIAN_DAY.
Constants.JULIAN_DAY.
KeplerianOrbit.KeplerianOrbit(double, double, double,
double, double, double, PositionAngle, Frame, AbsoluteDate, double)
Kurtosis identical
to the original
g constant in the Lanczos approximation, see
Gamma.lanczos(double).
lcm(a,b) = (a / gcd(a,b)) * b.
lcm(a,b) = (a / gcd(a,b)) * b.
vectorial objective functions to
scalar objective functions
when the goal is to minimize them.integrate method will perform an integration on the natural interval
[-1 , 1].
integrate method will perform an integration on the given interval.
IterativeLegendreGaussIntegrator instead.integrate method will perform an integration on the natural interval
[-1 , 1].
integrate method will perform an integration on the given interval.
DECIMAL128.
other contructor.
other contructor.
other contructor.
other contructor.
linear constraints.a(t -t0) + b.a * (t - t0) + b
using input Parameter and initial date.
List.InputStream.
LoessInterpolator
with a bandwidth of LoessInterpolator.DEFAULT_BANDWIDTH,
LoessInterpolator.DEFAULT_ROBUSTNESS_ITERS robustness iterations
and an accuracy of {#link #DEFAULT_ACCURACY}.
LoessInterpolator
with given bandwidth and number of robustness iterations.
LoessInterpolator
with given bandwidth, number of robustness iterations and accuracy.
LofOffset.LofOffset(Frame, LOFType)
LofOffset.LofOffset(Frame, LOFType, RotationOrder, double, double, double)
log(1 + p) function.Beta.logBeta(double, double).
normally distributed natural
logarithm of the log-normal distribution are equal to zero and one
respectively.
long.
first order
differential equations in order to compute exactly the main state jacobian
matrix for partial derivatives equations.OrbitTypes.mapOrbitToArray.
Parameter.
CycleCrossover.crossover(Chromosome, Chromosome).
OrderedCrossover.crossover(Chromosome, Chromosome).
NullArgumentException) inherit from this class.vector u such as : M(u) * v = u^v
Max identical
to the original
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
Mean identical
to the original
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
PositionAngle
PositionAngle
PositionAngle
KalmanFilter.Median identical
to the original
values array.
values
array, starting with the element in (0-based) position begin
in the array and including length values
Collection of Frequency objects into this instance.
UpdatingMultipleLinearRegression interface.Min identical
to the original
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
CodingEventDetector instance and returns an EventDetector instance that will trigger this
CodedEventsLogger every time eventOccurred is called.
MultiCodingEventDetector instance and returns an MultiEventDetector instance that will
trigger this MultiCodedEventsLogger every time
eventOccurred is called.
MSISE2000 Atmosphere model.AbstractDetector and adapted to
multi propagation.AdaptedStepHandler and adapted to multi
propagation.CodedEventsLogger and adapted to multi propagation.CodingEventDetector and adapted to multi propagation.EphemerisModeHandler and adapted to multi
propagation.EventDetector and adapted to multi propagation.EventsLogger and adapted to multi propagation.GenericCodingEventDetector and adapted to multi
propagation.MultiGenericCodingEventDetector that supports a Phenomenon.MultiGenericCodingEventDetector that supports a Phenomenon.MultiGenericCodingEventDetector that does not
support a Phenomenon.
MultiGenericCodingEventDetector that does not
support a Phenomenon.ModeHandler and adapted to multi propagation.NumericalPropagator and
adapted to multi propagation.OrekitFixedStepHandler and adapted to multi
propagation.OrekitStepHandler and adapted to multi
propagation.OrekitStepInterpolator and adapted to multi
propagation.OrekitStepNormalizer and adapted to multi
propagation.ResizableDoubleArray.ExpansionMode.MULTIPLICATIVE instead.
FunctionUtils.multiply(UnivariateDifferentiableFunction...)
Complex whose value is this * factor.
Complex whose value is this * factor, with factor
interpreted as a integer number.
Complex whose value is this * factor, with factor
interpreted as a real number.
BigInteger, returning the result in reduced form.
m.
this by m.
m.
this by m.
m.
this by m.
this by m.
m.
this by m.
this by m.
this by m.
m.
this by m.
m.
this by m.
m.
m.
this by m.
this matrix by the
specified value.
this matrix by the
specified value.
this matrix by the
specified value.
this matrix by the
specified value.
this matrix by the
specified value.
this matrix by the
specified value.
this matrix by the
specified value.
Propagator and adapted to multi propagation.UnivariateOptimizer interface
adding multi-start features to an existing optimizer.MultivariateFunction representing a
multivariate differentiable real function.MultivariateVectorFunction representing a
multivariate differentiable vectorial function.MultivariateFunction to unbounded ones.MultivariateFunction to an unbouded
domain using a penalty function.addValue method.Double.NaN as a Decimal64.
n.
Complex whose value is (-this).
this element.
this element.
this element.
Double.NEGATIVE_INFINITY as a
Decimal64.
Dfp with a value of 0.
Dfp given a String representation.
Dfp with a non-finite value.
this is, with a given arrayRepresentation.
Parameter.
Parameter.
NewtonRaphsonSolverBeta Distribution.
Beta Distribution.
Binomial Distribution.
Binomial Distribution.
boolean value from this random number generator's
sequence.
boolean value from this random number generator's
sequence.
boolean value from this random number generator's
sequence.
boolean value from this random number generator's
sequence.
boolean value from this random number generator's
sequence.
Cauchy Distribution.
Cauchy Distribution.
ChiSquare Distribution.
ChiSquare Distribution.
double value between 0.0 and
1.0 from this random number generator's sequence.
double value between 0.0 and
1.0 from this random number generator's sequence.
double value between 0.0 and
1.0 from this random number generator's sequence.
double value between 0.0 and
1.0 from this random number generator's sequence.
double value between 0.0 and
1.0 from this random number generator's sequence.
F Distribution.
F Distribution.
float
value between 0.0 and 1.0 from this random
number generator's sequence.
float
value between 0.0 and 1.0 from this random
number generator's sequence.
float
value between 0.0 and 1.0 from this random
number generator's sequence.
float
value between 0.0 and 1.0 from this random
number generator's sequence.
float
value between 0.0 and 1.0 from this random
number generator's sequence.
Gamma Distribution.
Gamma Distribution.
double value with mean 0.0 and standard
deviation 1.0 from this random number generator's sequence.
double value with mean 0.0 and standard
deviation 1.0 from this random number generator's sequence.
double value with mean 0.0 and standard
deviation 1.0 from this random number generator's sequence.
double value with mean 0.0 and standard
deviation 1.0 from this random number generator's sequence.
double value with mean 0.0 and standard
deviation 1.0 from this random number generator's sequence.
len.
len.
len.
Hypergeometric Distribution.
Hypergeometric Distribution.
int
value from this random number generator's sequence.
int value
between 0 (inclusive) and the specified value (exclusive), drawn from
this random number generator's sequence.
int
value from this random number generator's sequence.
int
value from this random number generator's sequence.
lower
and upper (endpoints included).
lower
and upper (endpoints included).
lower
and upper (endpoints included).
int
value from this random number generator's sequence.
int
value from this random number generator's sequence.
long
value from this random number generator's sequence.
long
value from this random number generator's sequence.
long
value from this random number generator's sequence.
lower and upper (endpoints included).
lower and upper (endpoints included).
lower and upper (endpoints included).
long
value from this random number generator's sequence.
long
value from this random number generator's sequence.
Pascal Distribution.
Pascal Distribution.
k whose entries are selected
randomly, without repetition, from the integers 0, ..., n - 1
(inclusive).
k whose entries are selected
randomly, without repetition, from the integers 0, ..., n - 1
(inclusive).
k whose entries are selected
randomly, without repetition, from the integers 0, ..., n - 1
(inclusive).
k objects selected randomly from the
Collection c.
k objects selected randomly from the
Collection c.
k objects selected randomly from the
Collection c.
lower
and upper (endpoints included) from a secure random sequence.
lower
and upper (endpoints included) from a secure random sequence.
lower
and upper (endpoints included) from a secure random sequence.
lower and upper (endpoints included) from a secure random
sequence.
lower and upper (endpoints included) from a secure random
sequence.
lower and upper (endpoints included) from a secure random
sequence.
T Distribution.
T Distribution.
(lower, upper) (i.e., endpoints excluded).
(lower, upper) or the interval [lower, upper).
(lower, upper) (i.e., endpoints excluded).
(lower, upper) or the interval [lower, upper).
(lower, upper) (i.e., endpoints excluded).
(lower, upper) or the interval [lower, upper).
Weibull Distribution.
Weibull Distribution.
Zipf Distribution.
Zipf Distribution.
line search solver and
preconditioner.
preconditioner.
SimpleValueChecker.SimpleValueChecker()
line search solver and
preconditioner.
preconditioner.
RealLinearOperator is expected.RealLinearOperator
is expected.NPointCrossover policy using the given number of points.
Vector3DFunction representing the n-th derivative of the current vector function.Vector3DFunction representing the n-th derivative of the current vector function.
null argument must throw
this exception.SpacecraftState using numerical integration.Parameter.
Parameter.
OceanTidesCoefficientsProviderRealMatrix objects compatible with octave.
time scale.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale to instance.
TAIScale.
TAIScale.
TAIScale.
TAIScale.
TAIScale.
TAIScale.
TAIScale.
TAIScale.
TAIScale.
TAIScale.
TAIScale.
1d as a Decimal64.
EventDetector into a MultiEventDetector.Entry optimized for OpenMap.v.
v.
v.
this by the vector x.
v.
v.
v.
v.
v.
v.
v.
this by the vector x.
this by the vector x.
v.
v.
this operator
by the vector x (optional operation).
method.
method.
BaseAbstractMultivariateOptimizer.optimize(int,MultivariateFunction,GoalType,OptimizationData[])
instead.
BaseAbstractMultivariateVectorOptimizer.optimize(int,MultivariateVectorFunction,OptimizationData[])
instead.
optimize(int,MultivariateDifferentiableVectorFunction,OptimizationData...)
instead.
optimize(int,MultivariateDifferentiableVectorFunction,OptimizationData...)
instead.
BaseAbstractMultivariateOptimizer.optimize(int,MultivariateFunction,GoalType,OptimizationData[])
instead.
BaseAbstractMultivariateVectorOptimizer.optimizeInternal(int,MultivariateVectorFunction,OptimizationData[])
instead.
AbstractDifferentiableOptimizer.optimizeInternal(int,MultivariateDifferentiableFunction,GoalType,OptimizationData[])
instead.
MultivariateDifferentiableVectorFunction.
StelaEquinoctialOrbit from mean to osculating parameters, and reverse.orbital parameters types.OrekitException instances in RuntimeException.OrekitStepHandler instances into one.OrekitFixedStepHandler
into a OrekitStepHandler.function package contains function objects that wrap the
methods contained in Math, as well as common
mathematical functions such as the gaussian and sinc functions.minimize or
maximize
a scalar function, called the
objective
function.NumericalPropagator, as well as
some classical spacecraft models for surface forces (spherical, box and solar array ...).Frame class; it represents a dynamic orientation frame,
i.e.AttitudeFrame as the parent frame.
OrientationFrame as the parent frame.
TransformProvider for OrientationFrame; it provides, for a given date,
the transformation corresponding to the frame orientation with respect to the parent frame.polyhedrons sets outlines.sample1 and
sample2 is 0 in favor of the two-sided alternative that the
mean paired difference is not equal to 0, with significance level
alpha.
IParamDiffFunction.partial derivatives equations.partial derivatives equations.Complex object.
Complex object.
BigFraction object.
BigFraction object.
Fraction object.
Fraction object.
BigFraction object.
Fraction object.
Vector object.
Vector object.
Vector3D object.
Vector3D object.
Vector object.
Vector object.
Vector object.
Vector object.
RealMatrix object.
RealMatrix object.
RealVector object.
RealVector object.
OrbitFile.
OrbitFile.
OrbitFile.
OrbitFile.
source until a non-whitespace character is found.
source until a non-whitespace character is found.
source for an expected fixed string.
BigInteger.
source until a non-whitespace character is found.
source until a non-whitespace character is found.
source for a number.
additional equations computing the partial derivatives
of the state (orbit) with respect to initial state and force models parameters.spheroids.Parameter.
Parameter.
Covariance.
Percentile identical
to the original
pth percentile of the values
in the values array.
pth percentile of the values
in the values array, starting with the element in (0-based)
position begin in the array and including length
values.
Phenomenon.CodingEventDetector is used, via the
monitorDetector method.Phenomenon instance.CodedEvent boundaries can be in any time order.
TrigonometricPolynomialFunction.
TrigonometricPolynomialFunction.
TrigonometricPolynomialFunction.
PolynomialFunction.
TrigonometricPolynomialFunction.
TrigonometricPolynomialFunction.
TrigonometricPolynomialFunction.
curve fitting.PolynomialFitter.PolynomialFitter(DifferentiableMultivariateVectorOptimizer) instead.
FourierSeries.
FourierSeries.
TrigonometricPolynomialFunction
TrigonometricPolynomialFunction
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
Double.POSITIVE_INFINITY as a
Decimal64.
EventDetector classes in Orekit:
for some events, g is positive when its associated phenomenon is active,
and for others, g is positive when its phenomenon is not active.MultiEventDetector classes in Patrius:
for some events, g is positive when its associated phenomenon is active,
and for others, g is positive when its phenomenon is not active.DerivativeStructure
x.
x.
BigFraction whose value is
(this<sup>exponent</sup>), returning the result in reduced form.
BigFraction whose value is
(thisexponent), returning the result in reduced form.
BigFraction whose value is
(thisexponent), returning the result in reduced form.
double whose value is
(thisexponent), returning the result in reduced form.
p times.
this with itself p
times.
p times.
this with itself p
times.
FramesConfigurationImplementation class.FramesFactory.y value associated with the
supplied x value, based on the data that has been
added to the model when this method is activated.
m.
v.
v.
this by m.
v.
v.
v.
v.
v.
v.
v.
m.
v.
v.
this by m.
v.
v.
TrigonometricPolynomialFunction
TrigonometricPolynomialFunction
X whose values are distributed according
to this distribution, this method returns P(x0 < X <= x1).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(x0 < X <= x1).
X whose values are distributed according
to this distribution, this method returns P(x0 < X <= x1).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(X = x).
X whose values are distributed according
to this distribution, this method returns P(X = x).
KalmanFilter.Product identical
to the original
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
ExtendedOneAxisEllipsoid class and provides utility methods needed for projections.true if IterativeLinearSolverEvent.getResidual() is supported.
true if IterativeLinearSolverEvent.getResidual() is supported.
FieldVector3D<DerivativeStructure>.
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
Parameter.
Parameter.
java.util.Random wrapping a
RandomGenerator.length.
AbstractIntegerDistribution.random instance variable instead.
AbstractRealDistribution.random instance variable instead.
RandomDataGenerator directlyRandomData interface using a RandomGenerator
instance to generate non-secure data and a SecureRandom
instance to provide data for the nextSecureXxx methods.RandomGenerator as
the source of (non-secure) random data.
RandomDataGenerator insteadRandomGenerator as
the source of (non-secure) random data.
java.util.Random.RandomKeys.data using the natural ordering on Doubles, with
NaN values handled according to nanStrategy and ties
resolved using tiesStrategy.
double)
vector spaces.nxm matrix in components list format
"{{a00,a01, ...,
a0m-1},{a10,
a11, ..., a1m-1},{...},{
an-10, an-11, ...,
an-1m-1}}".this element.
this element.
this element.
this element.
this element.
this element.
this element.
BigFraction to its lowest terms.
|a - offset| to the primary interval
[0, |period|).
Region.LinearConstraint.ConstantAttitudeLaw, or an ExtrapolatedAttitudeLaw (private class)CodedEvent to the list.
Phenomenon to the list.
data.
this object.
DataProvidersManager.removeProvider(DataProvider)
delta close to originalDelta with
the property that
EmpiricalDistribution.getNextValue().
System.currentTimeMillis() + System.identityHashCode(this)).
System.currentTimeMillis() + System.identityHashCode(this)).
valuesFileURL.
DoubleArray implementation that automatically
handles expanding and contracting its internal storage array as elements
are added and removed.double[] with the
initial capacity and numElements corresponding to the size of
the supplied double[] array.
ResizableDoubleArray.ResizableDoubleArray(int,double) instead.
ResizableDoubleArray.ResizableDoubleArray(int,double,double) instead.
ResizableDoubleArray.ResizableDoubleArray(int,double,double,ExpansionMode,double[])
instead.
UnivariateDifferentiableFunction implementation,
since this class uses a specific differentiation algorithm,
the returned DerivativeStructure instances are constant
( they cannot provide derivatives other than the first order already computed when they are created).rint function.RombergIntegrator.ROMBERG_MAX_ITERATIONS_COUNT)
n-th roots of
unity.n-th roots of unity.
Attitude.interpolate(AbsoluteDate, Collection)
or Attitude.slerp(AbsoluteDate, Attitude, Attitude, Frame, boolean)RungeKutta6Integrator.1 / SAFE_MIN does not overflow.
SatelliteInformation object with a given
satellite id.
SatelliteTimeCoordinate instance with
a given epoch and coordinate.
SatelliteTimeCoordinate object with a given epoch
and position coordinate.
SatelliteTimeCoordinate instance with a given
epoch, coordinate and clock value / rate change.
Propagator).
Propagator).
Propagator).
MultiPropagator).
MultiPropagator).
MultiPropagator).
TrigonometricPolynomialPrimitive
d to each entry of this.
d to each entry of this.
d to each entry of this.
TrigonometricPolynomialPrimitive by a scalar
d.
this by
d.
d.
this by
d.
d.
this by
d.
this by
d.
ISearchIndex.SearchIndexIntervalConvention.SecondMoment identical
to the original
biasCorrected
property and default (Downside) varianceDirection property.
biasCorrected
property and default (Downside) varianceDirection property.
Direction property
and default (true) biasCorrected property
isBiasCorrected
property and the specified Direction property.
SemiVariance identical
to the original
continue
propagation when entering the zone and to stop
when exiting the zone.
continue
propagation when entering the zone and to stop when exiting the zone.
continue
propagation when entering the zone and to stop when exiting the zone.
continue
propagation when entering the zone and to stop when exiting the zone.
size integers starting at start,
skipping stride numbers.
RealMatrix.
RealVector.
NumericalPropagator.setAttitudeProvider(AttitudeProvider)
ListPopulation.addChromosomes(Collection) instead
column
as a column matrix.
column of this matrix to the entries
of the specified array.
column
as a column matrix.
column of this matrix to the entries
of the specified array.
column
as a column matrix.
column of this matrix to the entries
of the specified array.
column
as a column matrix.
column of this matrix to the entries
of the specified column matrix.
column
as a column matrix.
column of this matrix to the entries
of the specified column matrix.
column
as a column matrix.
column of this matrix to the entries
of the specified column matrix.
column
as a vector.
column of this matrix to the entries
of the specified vector.
column
as a vector.
column of this matrix to the entries
of the specified vector.
column
as a vector.
column of this matrix to the entries
of the specified vector.
ResizableDoubleArray.setExpansionMode(ExpansionMode) instead.
UnivariateFunction to decompose and its period.
UnivariateIntegrator to use for the serires coefficient computation.
mean used in data generation.
MultiNumericalPropagator.addInitialState(SpacecraftState, String) method
before defining the associated integration frame.
SP3File.SP3OrbitType for this SP3 file.
DescriptiveStatistics.getPercentile(double).
index.
index.
row
as a row matrix.
row of this matrix to the entries
of the specified array.
row
as a row matrix.
row of this matrix to the entries
of the specified array.
row
as a row matrix.
row of this matrix to the entries
of the specified array.
row
as a row matrix.
row of this matrix to the entries of
the specified row matrix.
row
as a row matrix.
row
as a row matrix.
row of this matrix to the entries of
the specified row matrix.
row
as a row matrix.
row
as a row matrix.
row of this matrix to the entries of
the specified row matrix.
row
as a vector.
row of this matrix to the entries of
the specified vector.
row
as a vector.
row of this matrix to the entries of
the specified vector.
row
as a vector.
row of this matrix to the entries of
the specified vector.
int seed.
int array seed.
long seed.
int seed.
int array seed.
long seed.
int seed.
long seed.
int array seed.
int seed.
int array seed.
int seed.
int array seed.
long seed.
int seed.
int array seed.
long seed.
int seed.
int array seed.
long seed.
standard deviation used in ValueServer.GAUSSIAN_MODE.
BaseAbstractMultivariateOptimizer.optimize(int,MultivariateFunction,GoalType,OptimizationData[])
method.
(row, column) using data in the
input subMatrix array.
row, column using data in the
input subMatrix array.
(row, column) using data in the
input subMatrix array.
row, column using data in the
input subMatrix array.
(row, column) using data in the
input subMatrix array.
row, column using data in the
input subMatrix array.
row, column using data in the
input subMatrix array.
(row, column) using data in the
input subMatrix array.
row, column using data in the
input subMatrix array.
row, column using data in the
input subMatrix array.
PVCoordinatesProvider
input parsed by this base
class.
input parsed by this base
class.
values file URL using a string
URL representation.
values file URL.
Ps(x)
whose values at point x will be the same as the those from the
original polynomial P(x) when computed at x + shift.
Orbit.orbitShiftedBy(double) implemented in inherited classes of Orbit.
short.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventHandler.eventOccurred(double, double[], boolean, boolean) has been called.
EventHandler.eventOccurred(double, double[], boolean, boolean) has been called.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventHandler.eventOccurred(double, double[], boolean, boolean) has been called.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventHandler.eventOccurred(double, double[], boolean, boolean) has been called.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
MultiEventDetector.eventOccurred(java.util.Map, boolean, boolean) has been called.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
hyperplane of a space.signum function.MassProvider.ConvergenceChecker interface using
only point coordinates.AbstractConvergenceChecker.AbstractConvergenceChecker()
ConvergenceChecker interface
that uses only objective function values.AbstractConvergenceChecker.AbstractConvergenceChecker()
ConvergenceChecker interface using
only objective function values.AbstractConvergenceChecker.AbstractConvergenceChecker()
ConvergenceChecker interface using
only objective function values.AbstractConvergenceChecker.AbstractConvergenceChecker()
SimpleValueChecker.SimpleValueChecker()
sin(x) / x.
Skewness identical
to the original
Attitude.interpolate(AbsoluteDate, Collection) or
Attitude.slerp(AbsoluteDate, Attitude, Attitude, Frame, boolean)solar activity data providersParameter.
startValue.
startValue.
startValue.
startValue.
startValue.
startValue.
startValue.
startValue.
min and max.
min and max.
startValue.
AbstractIntegerDistribution.inverseCumulativeProbability(double).
RealMatrix.
RealMatrix.
SpacecraftState.toTransform()SphericalCap using a Sphere and a Plane.
Dfp into 2 Dfp's such that their sum is equal to the input Dfp.
this diagonal operator.
1 - this2 for this complex
number.
StandardDeviation identical
to the original
isBiasCorrected property.
isBiasCorrected property and the supplied external moment.
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
Propagator methods for analytical propagators.EquinoctialParameters parameters.StelaGTOPropagator.additional equations computing the partial
derivatives of the state (orbit) with respect to initial state.FixedStepHandler
into a StepHandler.Step normalizer bounds settings.Step normalizer modes.S(n,k)", the number of
ways of partitioning an n-element set into k non-empty
subsets.
UnivariateStatistic with
StorelessUnivariateStatistic.increment(double) and StorelessUnivariateStatistic.incrementAll(double[]) methods for adding
values and updating internal state.split method.Line.Line.OrientedPoint.Plane.value for the most recently added value.
TrigonometricPolynomialPrimitive
PolynomialFunction
TrigonometricPolynomialFunction
Complex whose value is
(this - subtrahend).
Complex whose value is
(this - subtrahend).
BigInteger from the value of this
BigFraction, returning the result in reduced form.
integer from the value of this
BigFraction, returning the result in reduced form.
long from the value of this
BigFraction, returning the result in reduced form.
m from this matrix.
this minus m.
m from this matrix.
this minus m.
this minus v.
this minus v.
v from this vector.
m from this matrix.
this - m.
this minus m.
m from this matrix.
this minus m.
this minus m.
m from this matrix.
this minus v.
this minus m.
m from this matrix.
v from this vector.
this minus m.
v from this vector.
this minus v.
this minus v.
m.
m.
this minus m.
Sum identical
to the original
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
addValue method.SumOfLogs identical
to the original
SumOfSquares identical
to the original
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
DescriptiveStatistics that
is safe to use in a multithreaded environment.MultivariateSummaryStatistics that
is safe to use in a multithreaded environment.RandomGenerator implementation can be thread-safe if it
is used through an instance of this class.RandomGenerator
instance.
SummaryStatistics that
is safe to use in a multithreaded environment.sampleStats to mu.
StatisticalSummary instances, without the
assumption of equal subpopulation variances.
TabulatedAttitude.TabulatedAttitude(List) or TabulatedAttitude.TabulatedAttitude(List, int)
TargetPointing does not guarantee the
target point belongs to the body surface, this class always provides a ground point target.Parameter.
Parameter.
evaluate(double[], int, int) methods
to verify that the input parameters designate a subarray of positive length.
evaluate(double[], int, int) methods
to verify that the input parameters designate a subarray of positive length.
evaluate(double[], double[], int, int) methods
to verify that the begin and length parameters designate a subarray of positive length
and the weights are all non-negative, non-NaN, finite, and not all zero.
evaluate(double[], double[], int, int) methods
to verify that the begin and length parameters designate a subarray of positive length
and the weights are all non-negative, non-NaN, finite, and not all zero.
CodedEventsLogger, generating the list of detected events and
the list of corresponding phenomena.AbsoluteDate
date attached to them.time-stamped version of AngularCoordinates.time-stamped data.TimeStampedCache.time stamped caches.time-stamped version of PVCoordinates.FieldVector3D<DerivativeStructure>.
doubles.
doubles.
doubles.
Date.
FieldVector3D<DerivativeStructure>.
DifferentiableMultivariateFunction interface itself is deprecated
DifferentiableMultivariateVectorFunction interface itself is deprecated
DifferentiableUnivariateFunction interface itself is deprecated
StelaEquinoctialOrbit to a mean one.
DifferentiableMultivariateFunction interface itself is deprecated
DifferentiableMultivariateFunction interface itself is deprecated
StelaEquinoctialOrbit to an osculating one.
String representing this fraction, ie
"num / dem" or just "num" if the denominator is one.
String representing this fraction, ie
"num / dem" or just "num" if the denominator is one.
String is equal to
Double.toString(this.doubleValue())
states.
DifferentiableUnivariateFunction interface itself is deprecated
PVCoordinates including kinematic effects from an algebraic point of view.
TimeStampedPVCoordinates including kinematic effects.
Tricubic interpolation in three dimensions
F.- TricubicSplineInterpolatingFunction(double[], double[], double[], double[][][], double[][][], double[][][], double[][][], double[][][], double[][][], double[][][], double[][][]) - Constructor for class org.apache.commons.math3.analysis.interpolation.TricubicSplineInterpolatingFunction
- TricubicSplineInterpolator - Class in org.apache.commons.math3.analysis.interpolation
- Generates a tricubic interpolating function.
- TricubicSplineInterpolator() - Constructor for class org.apache.commons.math3.analysis.interpolation.TricubicSplineInterpolator
- trigamma(double) - Static method in class org.apache.commons.math3.special.Gamma
- Computes the trigamma function of x.
- trigger(int) - Method in interface org.apache.commons.math3.util.Incrementor.MaxCountExceededCallback
- Function called when the maximal count has been reached.
- TrigonometricPolynomialFunction - Class in org.apache.commons.math3.analysis.polynomials
- This class is the Trigonometric Polynomial Function class.
- TrigonometricPolynomialFunction(double, double[], double[]) - Constructor for class org.apache.commons.math3.analysis.polynomials.TrigonometricPolynomialFunction
- Constructor for the
TrigonometricPolynomialFunction.- TrigonometricPolynomialPrimitive - Class in org.apache.commons.math3.analysis.polynomials
- This class represents a trigonometric polynomial primitive.
- TrigonometricPolynomialPrimitive(PolynomialFunction, TrigonometricPolynomialFunction) - Constructor for class org.apache.commons.math3.analysis.polynomials.TrigonometricPolynomialPrimitive
- Constructor for the
TrigonometricPolynomialPrimitiveclass- TriLinearIntervalsFunction - Class in org.apache.commons.math3.analysis.interpolation
- Implements the representation of a linear function in dimension 2.
- TriLinearIntervalsFunction(double[], double[], double[], double[][][]) - Constructor for class org.apache.commons.math3.analysis.interpolation.TriLinearIntervalsFunction
- Constructor, in three dimensions.
- TriLinearIntervalsFunction(ISearchIndex, ISearchIndex, ISearchIndex, double[][][]) - Constructor for class org.apache.commons.math3.analysis.interpolation.TriLinearIntervalsFunction
- Constructor, in three dimensions with a search index algorithm as a parameter.
- TriLinearIntervalsInterpolator - Class in org.apache.commons.math3.analysis.interpolation
- Class representing a TrivariateGridInterpolator for linear interpolation in dimension 3.
- TriLinearIntervalsInterpolator() - Constructor for class org.apache.commons.math3.analysis.interpolation.TriLinearIntervalsInterpolator
- TrivariateFunction - Interface in org.apache.commons.math3.analysis
- An interface representing a trivariate real function.
- TrivariateGridInterpolator - Interface in org.apache.commons.math3.analysis.interpolation
- Interface representing a trivariate real interpolating function where the sample points must be specified on a regular grid.
- TroposphericCorrection - Interface in org.orekit.models.earth
- Defines a tropospheric model, used to calculate the signal delay for the signal path imposed to electro-magnetic signals between an orbital satellite and a ground station.
- TRUE_ANOMALY - Static variable in class org.orekit.orbits.KeplerianOrbit
- Deprecated. as of 6.0 replaced by
PositionAngle- TRUE_LATITUDE_ARGUMENT - Static variable in class org.orekit.orbits.EquinoctialOrbit
- Deprecated. as of 6.0 replaced by
PositionAngle- TRUE_LONGITUDE_ARGUMENT - Static variable in class org.orekit.orbits.CircularOrbit
- Deprecated. as of 6.0 replaced by
PositionAngle- trunc(DfpField.RoundingMode) - Method in class org.apache.commons.math3.dfp.Dfp
- Does the integer conversions with the specified rounding.
- tselec() - Method in class org.orekit.forces.atmospheres.MSIS2000.Flags
- Prepare sw and swc.
- tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
- tsi from SPTRCK #3.
- tTest(double, double[], double) - Static method in class org.apache.commons.math3.stat.inference.TestUtils
- tTest(double, double[]) - Static method in class org.apache.commons.math3.stat.inference.TestUtils
- tTest(double, StatisticalSummary, double) - Static method in class org.apache.commons.math3.stat.inference.TestUtils
- tTest(double, StatisticalSummary) - Static method in class org.apache.commons.math3.stat.inference.TestUtils
- tTest(double[], double[], double) - Static method in class org.apache.commons.math3.stat.inference.TestUtils
- tTest(double[], double[]) - Static method in class org.apache.commons.math3.stat.inference.TestUtils
- tTest(StatisticalSummary, StatisticalSummary, double) - Static method in class org.apache.commons.math3.stat.inference.TestUtils
- tTest(StatisticalSummary, StatisticalSummary) - Static method in class org.apache.commons.math3.stat.inference.TestUtils
- TTest - Class in org.apache.commons.math3.stat.inference
- An implementation for Student's t-tests.
- TTest() - Constructor for class org.apache.commons.math3.stat.inference.TTest
- tTest(double, double[]) - Method in class org.apache.commons.math3.stat.inference.TTest
- Returns the observed significance level, or p-value, associated with a one-sample, two-tailed t-test comparing the mean of the input array with the constant
mu.- tTest(double, double[], double) - Method in class org.apache.commons.math3.stat.inference.TTest
- Performs a two-sided t-test evaluating the null hypothesis that the mean of the population from which
sampleis drawn equalsmu.- tTest(double, StatisticalSummary) - Method in class org.apache.commons.math3.stat.inference.TTest
- Returns the observed significance level, or p-value, associated with a one-sample, two-tailed t-test comparing the mean of the dataset described by
sampleStatswith the constantmu.- tTest(double, StatisticalSummary, double) - Method in class org.apache.commons.math3.stat.inference.TTest
- Performs a two-sided t-test evaluating the null hypothesis that the mean of the population from which the dataset described by
statsis drawn equalsmu.- tTest(double[], double[]) - Method in class org.apache.commons.math3.stat.inference.TTest
- Returns the observed significance level, or p-value, associated with a two-sample, two-tailed t-test comparing the means of the input arrays.
- tTest(double[], double[], double) - Method in class org.apache.commons.math3.stat.inference.TTest
- Performs a two-sided t-test evaluating the null hypothesis that
sample1andsample2are drawn from populations with the same mean, with significance levelalpha.- tTest(StatisticalSummary, StatisticalSummary) - Method in class org.apache.commons.math3.stat.inference.TTest
- Returns the observed significance level, or p-value, associated with a two-sample, two-tailed t-test comparing the means of the datasets described by two StatisticalSummary instances.
- tTest(StatisticalSummary, StatisticalSummary, double) - Method in class org.apache.commons.math3.stat.inference.TTest
- Performs a two-sided t-test evaluating the null hypothesis that
sampleStats1andsampleStats2describe datasets drawn from populations with the same mean, with significance levelalpha.- tTest(double, double, double, double) - Method in class org.apache.commons.math3.stat.inference.TTest
- Computes p-value for 2-sided, 1-sample t-test.
- tTest(double, double, double, double, double, double) - Method in class org.apache.commons.math3.stat.inference.TTest
- Computes p-value for 2-sided, 2-sample t-test.
- TTScale - Class in org.orekit.time
- Terrestrial Time as defined by IAU(1991) recommendation IV.
- TWELVE - Static variable in class org.orekit.forces.atmospheres.solarActivity.specialized.AbstractMSISE2000SolarData
- Constant 12
- TWO - Static variable in class org.apache.commons.math3.fraction.BigFraction
- A fraction representing "2 / 1".
- TWO - Static variable in class org.apache.commons.math3.fraction.Fraction
- A fraction representing "2 / 1".
- TWO_FIFTHS - Static variable in class org.apache.commons.math3.fraction.BigFraction
- A fraction representing "2/5".
- TWO_FIFTHS - Static variable in class org.apache.commons.math3.fraction.Fraction
- A fraction representing "2/5".
- TWO_PI - Static variable in class org.apache.commons.math3.util.MathUtils
- 2 π.
- TWO_QUARTERS - Static variable in class org.apache.commons.math3.fraction.BigFraction
- A fraction representing "2/4".
- TWO_QUARTERS - Static variable in class org.apache.commons.math3.fraction.Fraction
- A fraction representing "2/4".
- TWO_THIRDS - Static variable in class org.apache.commons.math3.fraction.BigFraction
- A fraction representing "2/3".
- TWO_THIRDS - Static variable in class org.apache.commons.math3.fraction.Fraction
- A fraction representing "2/3".
- TwoDirectionsAttitude - Class in org.orekit.attitudes
- This class implements a generic two directions attitude law.
- TwoDirectionsAttitude(IDirection, IDirection, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.TwoDirectionsAttitude
- Constructor.
- TwoSpinBiasSlew - Class in org.orekit.attitudes
- This class extends the AbstractSlew.
- TwoSpinBiasSlew(AttitudeProvider, AttitudeProvider, AbsoluteDate, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.attitudes.TwoSpinBiasSlew
- This class extends the AbstractSlew.
ulp function.RandomVectorGenerator that generates vectors with uncorrelated
components.UniformCrossover policy using the given mixing ratio.
RandomVectorGenerator that generates vectors with with
correlated components.MersenneTwister),
in order to generate the individual components.
Dfp function.UnivariateMatrixFunction representing a univariate differentiable matrix function.UnivariateVectorFunction representing a univariate differentiable vectorial function.UnivariateInterpolator
interface.UnivariateSolver objects.OrekitException.
ExceptionContextProvider.
OrekitException.
ExceptionContextProvider.
AbstractLeastSquaresOptimizer.computeWeightedJacobian(double[])
instead.
Transform
as an input argument.
Transform as an input argument.
AbstractLeastSquaresOptimizer.computeResiduals(double[]),
BaseAbstractMultivariateVectorOptimizer.computeObjectiveValue(double[]), AbstractLeastSquaresOptimizer.computeCost(double[])
and AbstractLeastSquaresOptimizer.setCost(double) instead.
FramesFactory.getMOD(boolean) to provided frame.
FramesFactory.getMOD(boolean) to provided frame.
X, this method returns P(X >= x).
x.
x.
x.
x.
x.
ValueServer.ValueServer(RandomGenerator)
AttitudeLegsSequence, using a variable time step.LocalOrbitalFrame.
LocalOrbitalFrame.
isBiasCorrected
property.
isBiasCorrected
property
isBiasCorrected
property and the supplied external second moment.
Variance identical
to the original
Double.NaN if the array is empty.
Double.NaN if the designated subarray
is empty.
lower < initial < upper.
lower < initial < upper.
curve fitting.AbstractLeastSquaresOptimizer.computeWeightedJacobian(double[]) instead.
0d as a Decimal64.
|
||||||||||
| PREV NEXT | FRAMES NO FRAMES | |||||||||