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- User Manual 3.4.1 Numerical ordinary differential equations
- User Manual 3.4.1 Parallelepipeds
- User Manual 3.4.1 Planes
- User Manual 3.4.1 Plates
- User Manual 3.4.1 Projections
- User Manual 3.4.1 Properties and models: Inertia
- User Manual 3.4.1 Rectangular cone
- User Manual 3.4.1 Right circular cone
- User Manual 3.4.1 Right circular cylinder
- User Manual 3.4.1 Rotations and quaternions
- User Manual 3.4.1 Spheres
- User Manual 3.4.1 Spherical Caps
- User Manual 3.4.1 Spheroids
- User Manual 3.4.1 The Cone Interface
- User Manual 3.4.1 The Cylinder Interface
- User Manual 3.4.1 The Infinite Cone Interface
- User Manual 3.4.1 The Infinite Cylinder Interface
- User Manual 3.4.1 Time
- User Manual 4.0 Angles and Intervals
- User Manual 4.0 Assemblies in PATRIUS: Building and using an assembly
- User Manual 4.0 Assemblies in PATRIUS: Presentation
- User Manual 4.0 Attitude ephemeris
- User Manual 4.0 Attitude law
- User Manual 4.0 Attitude leg
- User Manual 4.0 Celestial bodies
- User Manual 4.0 Directions
- User Manual 4.0 Environment Models
- User Manual 4.0 Errors management and internationalization
- User Manual 4.0 Events: ground stations and satellites
- User Manual 4.0 Events detection: Presentation
- User Manual 4.0 Facets
- User Manual 4.0 Frames
- User Manual 4.0 Frames configuration
- User Manual 4.0 Guidance commands
- User Manual 4.0 Kinematics
- User Manual 4.0 Matrices
- User Manual 4.0 Measure and Filtering
- User Manual 4.0 Multi Propagation
- User Manual 4.0 Multi events detection
- User Manual 4.0 Numerical ordinary differential equations
- User Manual 4.0 Numerical propagation
- User Manual 4.0 Orbital parameters
- User Manual 4.0 Parallelepipeds
- User Manual 4.0 Plates
- User Manual 4.0 Projections
- User Manual 4.0 Properties and models: Inertia
- User Manual 4.0 Rotation, AngularCoordinates, Tranform and Attitude : how to use them
- User Manual 4.0 Rotations and quaternions
- User Manual 4.0 SpacecraftState
- User Manual 4.0 The Cone Interface