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WSF
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A target point with kinematics given by a propagator. More...
#include <WsfPropagatorTargetPoint.hpp>


Public Member Functions | |
| PropagatorTargetPoint (std::unique_ptr< UtOrbitalPropagatorBase > aPropPtr) | |
| PropagatorTargetPoint (const PropagatorTargetPoint &aOther) | |
| PropagatorTargetPoint & | operator= (const PropagatorTargetPoint &aOther)=delete |
| ~PropagatorTargetPoint () override=default | |
| PropagatorTargetPoint * | Clone () const override |
| Create a copy of this target point. | |
| void | Update (const UtCalendar &aEpoch) override |
Update the point to the given aEpoch. | |
| ut::OrbitalStateVector | GetOrbitalStateVectorInertial () const override |
| Return the combined inertial position and velocity of this point at this object's current epoch. | |
| UtVec3d | GetPositionECI () const override |
| Return the ECI position of this point at this object's current epoch. | |
| UtVec3d | GetVelocityECI () const override |
| Return the ECI velocity of this point at this object's current epoch. | |
| UtCalendar | GetEpoch () const override |
| Return the current epoch of this point. | |
| double | GetCharacteristicTime () const override |
| Public Member Functions inherited from wsf::space::OrbitalTargetPoint | |
| OrbitalTargetPoint ()=default | |
| virtual | ~OrbitalTargetPoint ()=default |
A target point with kinematics given by a propagator.
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inlineexplicit |
Referenced by Clone(), operator=(), and PropagatorTargetPoint().
| wsf::space::PropagatorTargetPoint::PropagatorTargetPoint | ( | const PropagatorTargetPoint & | aOther | ) |
References PropagatorTargetPoint().
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overridedefault |
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inlineoverridevirtual |
Create a copy of this target point.
Implements wsf::space::OrbitalTargetPoint.
References PropagatorTargetPoint().
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overridevirtual |
Return a characteristic time for this point.
This is used in the Target maneuver to set a maximum search time when there is no user input for this value. This method should return a reasonable time that likely includes the targeting solution. For example, a propagator based OrbitalTargetPoint might return the orbital period.
Implements wsf::space::OrbitalTargetPoint.
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overridevirtual |
Return the current epoch of this point.
Implements wsf::space::OrbitalTargetPoint.
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overridevirtual |
Return the combined inertial position and velocity of this point at this object's current epoch.
Implements wsf::space::OrbitalTargetPoint.
Referenced by GetPositionECI(), and GetVelocityECI().
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overridevirtual |
Return the ECI position of this point at this object's current epoch.
Implements wsf::space::OrbitalTargetPoint.
References GetOrbitalStateVectorInertial().
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overridevirtual |
Return the ECI velocity of this point at this object's current epoch.
Implements wsf::space::OrbitalTargetPoint.
References GetOrbitalStateVectorInertial().
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delete |
References PropagatorTargetPoint().
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overridevirtual |
Update the point to the given aEpoch.
Implements wsf::space::OrbitalTargetPoint.
References Update().
Referenced by Update().