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- Examples:
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testEnvironment.cpp.
Definition at line 24 of file access.h.
Referenced by ab_Fmatrix(), ab_Hmatrix(), ab_measurementRHSFunc(), ab_Rmatrix(), ab_stateRHSFunc(), AttitudeTrajectory(), AttituteDynamics(), AttituteDynamics_QuaternionAngVel(), CAMvectorBase::CAMvectorBase(), QuaternionEKFObserver::CheckMagnetometerMeasurement(), O_SESSAME::TestKeplerian::DisplayPositionVelocity(), DragForceFunction(), OrbitController::ECEF2ECI(), OrbitObserver::ECEF2NEDVelocity(), OrbitController::ECEF2NEDVelocity(), OrbitObserver::ECEF2WGS84(), OrbitController::ECEF2WGS84(), OrbitController::ECI2ECEF(), triadObserver::GetAttitude(), QuaternionEKFObserver::GetCurrentMeasurements(), O_SESSAME::Quaternion::GetEulerAxisAngle(), SequentialFilterHistory::GetHistory(), O_SESSAME::OrbitHistory::GetHistory(), O_SESSAME::AttitudeHistory::GetHistory(), QuaternionEKFObserver::GetInitialGuessTriad(), KalmanFilterHistory::GetKalmanHistory(), Whorl::GetMRP(), Whorl::GetOmegaBL(), O_SESSAME::Keplerian::GetPositionVelocity(), Whorl::GetQuaternion(), Whorl::GetReferenceOmegaBL(), Whorl::GetReferenceQuaternion(), O_SESSAME::Rotation::GetRotation(), O_SESSAME::PositionVelocity::GetState(), O_SESSAME::AttitudeState::GetState(), O_SESSAME::AttitudeHistory::GetState(), GravityForceFunction(), GravityGradientTorque(), Whorl::Initialize(), CAMvectorBase::initialize(), slidingModeControlMRPMW::Initialize(), COENaaszController::Initialize(), O_SESSAME::RungeKuttaIntegrator::Integrate(), Magnetometer::Magnetometer(), main(), matrixDet(), matrixInv3x3(), QuaternionEKFObserver::MeasurementUpdate(), QuaternionEKFObserver::MurrellAlgorithm(), myAttitudeStateConvFunc(), myOrbitStateConvFunc(), OrbitObserver::NED2ECEFVelocity(), OrbitController::NED2ECEFVelocity(), CAMvectorBase::operator+(), CAMmatrixBase::operator+(), operator+(), CAMarrayBase::operator+(), CAMvectorBase::operator+=(), CAMmatrixBase::operator+=(), CAMarrayBase::operator+=(), CAMvectorBase::operator-(), CAMmatrixBase::operator-(), operator-(), CAMarrayBase::operator-(), CAMvectorBase::operator-=(), CAMmatrixBase::operator-=(), CAMarrayBase::operator-=(), CAMvectorBase::operator=(), CAMmatrixBase::operator=(), CAMarrayBase::operator=(), CAMmatrixBase::operator~(), OrbitForcesFunctor(), OrbitForcesWithDragFunctor(), otimes(), param_Euler_Ematrix(), Plot(), PositionVelocityConvFunc(), O_SESSAME::CombinedNumericPropagator::PropagateAttitude(), O_SESSAME::CombinedNumericPropagator::PropagateOrbit(), qdot(), QuaternionAngVelConvFunc(), QuaternionDynamics(), AttitudeModels::QuaternionKinematic(), QuaternionKinematics(), Controller::ReferenceModelSC(), Controller::ReferenceTrajectory(), triadObserver::Run(), SingleAxisController::Run(), DefaultObserver::Run(), COENaaszController::Run(), AttitudeObserver::Run(), atterrbiasObserver::Run(), RungeKuttaSolve(), O_SESSAME::Quaternion::Set(), Whorl::SetAngularRateError(), O_SESSAME::Keplerian::SetKeplerianRepresentationEccentricAnomaly(), O_SESSAME::Keplerian::SetKeplerianRepresentationMeanAnomaly(), Whorl::SetMRPError(), O_SESSAME::Keplerian::SetPositionVelocity(), Whorl::SetReferenceOmegaBL(), Whorl::SetReferenceQuaternion(), O_SESSAME::PositionVelocity::SetState(), SetupAttitude(), SetupEnvironment(), PhysicalMomentumWheel::SetWheelSpeedCoefficients(), QuaternionEKFObserver::SingleMeasurement(), QuaternionEKFObserver::StateCovarianceUpdate(), QuaternionEKFObserver::StateTransitionMatrix(), ThirdBodyForceDisturbance(), CAMmatrixBase::transpose(), TwoBodyDynamics(), OrbitObserver::WGS842ECEF(), and OrbitController::WGS842ECEF(). |