Package org.orekit.attitudes
Some force models such as the atmospheric drag or the maneuvers need to
know the spacecraft orientation in inertial frame. OREKIT uses a simple
container for Attitude which
includes both the geometric part (i.e. rotation) and the kinematic part
(i.e. the instant spin axis). The components hold by this container
allow to convert vectors from inertial frame to spacecraft frame along
with their derivatives. This container is similar in spirit to the various
extensions of the abstract Orbit class:
it represents a state at a specific instant.
Several classical attitude laws are already provided in this package.
One special implementation is the AttitudesSequence class which
handle a set of laws, only one of which being active at any time. The
active law changes as switch events are triggered.

- Author:
- Fabien Maussion, Luc Maisonobe, Véronique Pommier-Maurussane
-
ClassDescriptionA
BoundedAttitudeProviderthat covers a larger time span from several constituent attitude providers that cover shorter time spans.Attitude provider with one satellite vector aligned and another one constrained to two targets.This class handles attitude definition at a given date.This interface represents a builder for attitude.Class for attitude interpolation.This interface represents an attitude provider model set.This interface represents an attitude provider that modifies/wraps another underlying provider.Interface for (attitude) rotation models taking as inputs a spacecraft state and model parameters.This classes manages a sequence of different attitude providers that are activated in turn according to switching events.This classes manages a sequence of different attitude providers that are activated in turn according to switching events.Interface for attitude switch notifications.This class handles body center pointing attitude provider.This interface is intended for attitude ephemerides valid only during a time range.This class handles a celestial body pointed attitude provider.FieldAttitude<T extends CalculusFieldElement<T>>This class handles attitude definition at a given date.FieldAttitudeInterpolator<KK extends CalculusFieldElement<KK>>Class for attitude interpolation.FieldInertia<T extends CalculusFieldElement<T>>Container for inertia of a 3D object.FieldInertiaAxis<T extends CalculusFieldElement<T>>Container for inertial axis.Builder that assumes angular coordinates are given in a fixed frame.This class handles a simple attitude provider at constant rate around a fixed axis.This class handles an attitude provider aligned with a frame or a fixed offset to it.Base class for ground pointing attitude providers.Abstract class for attitude provider modifiers using an underlying ground pointing law.Ground point target forAlignedAndConstrained.Container for inertia of a 3D object.Container for inertial axis.Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.This class provides a default attitude provider.This class handles nadir pointing attitude provider.Predefined targets forAlignedAndConstrained.This class handles a spin stabilized attitude provider.This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.This class handles an attitude provider interpolating from a predefined table.This class handles target pointing attitude provider.Provider for target vector.This class handles torque-free motion of a general (non-symmetrical) body.This class handles yaw compensation attitude provider.This class handles yaw steering law.