#include <WsfNonClassicalOrbitalPropagator.hpp>
◆ WsfNonClassicalOrbitalPropagator() [1/2]
| WsfNonClassicalOrbitalPropagator::WsfNonClassicalOrbitalPropagator |
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std::unique_ptr< ut::OrbitalState > | aInitialOrbitalStatePtr | ) |
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explicit |
◆ WsfNonClassicalOrbitalPropagator() [2/2]
◆ ~WsfNonClassicalOrbitalPropagator()
| WsfNonClassicalOrbitalPropagator::~WsfNonClassicalOrbitalPropagator |
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overridedefault |
◆ GetManeuveringPropagator()
| std::unique_ptr< UtOrbitalPropagatorBase > WsfNonClassicalOrbitalPropagator::GetManeuveringPropagator |
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const |
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override |
◆ operator=()
◆ SolveLambertProblem()
| UtLambertProblem::Result WsfNonClassicalOrbitalPropagator::SolveLambertProblem |
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const ut::CentralBody & | aCentralBody, |
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const UtVec3d & | aLocationECI_1, |
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const UtVec3d & | aLocationECI_2, |
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double | aDt, |
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bool | aShortWay, |
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bool | aAllowHitsEarth, |
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double | aConvergenceTolerance = 1.0e-12 ) const |
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override |
The documentation for this class was generated from the following files: