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- 2 septembre 2024 à 07:51 User Manual 4.14 Orbits (hist) [5 525 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === The "orbits" package contains classes to represent the orbital state of a spacecraft at a given time. Several types of orbits ar... »)
- 2 septembre 2024 à 07:50 User Manual 4.14 Orbital parameters (hist) [5 250 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === The "Orbital parameters" package contains classes to represent the orbital state of a space object. Several types of parameter... »)
- 2 septembre 2024 à 07:49 User Manual 4.14 Frames configuration (hist) [25 313 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === Frames configuration defines the models and data to use for each frame transformation. Several frames configurations are already... »)
- 2 septembre 2024 à 07:49 User Manual 4.14 Frames (hist) [17 176 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === In Patrius, a frame is represented by the class Frame. The different frames are organized as a tree whose root is the ICRF. A f... »)
- 2 septembre 2024 à 07:48 User Manual 4.14 Celestial bodies (hist) [33 088 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === The celestial bodies are described by their main features : position and geometry. The positions are ephemeris that must be loa... »)
- 2 septembre 2024 à 07:48 User Manual 4.14 Slew (hist) [6 241 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === A slew performs the transition between two attitude laws. === Javadoc === The attitude objects linked to slews are available i... »)
- 2 septembre 2024 à 07:46 User Manual 4.14 Rotation, AngularCoordinates, Tranform and Attitude : how to use them (hist) [15 871 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == In PATRIUS, several objects allow the user to represent rotations and perform some frame transformations, from simplest to most complex: * <c... »)
- 2 septembre 2024 à 07:46 User Manual 4.14 Orientation (hist) [3 381 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === The purpose of this chapter is to describe the orientation package. An orientation provider is an interface that provides meth... »)
- 2 septembre 2024 à 07:45 User Manual 4.14 Kinematics (hist) [10 115 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === The purpose is to extend the attitude package with classes and methods to compute and process kinematics operations. === Javad... »)
- 2 septembre 2024 à 07:45 User Manual 4.14 Directions (hist) [8 111 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === The “direction” objects are used for attitude computation purposes to describe different types of axis in space that can evo... »)
- 2 septembre 2024 à 07:44 User Manual 4.14 Attitude Profile (hist) [6 494 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === An attitude profile is an attitude law providing the computation of an instantaneous attitude without any reference to the satel... »)
- 2 septembre 2024 à 07:44 User Manual 4.14 Attitude leg (hist) [9 272 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === The purpose of this chapter is to describe the current Patrius attitude legs. An attitude leg is a time-bounded attitude law.... »)
- 2 septembre 2024 à 07:43 User Manual 4.14 Attitude law (hist) [22 748 octets] Admin tsn (discussion | contributions) (Page créée avec « __NOTOC__ == Introduction == === Scope === The purpose of this chapter is to describe the current Patrius attitude laws. === Javadoc === The attitude objects are availab... »)
