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| double | cqsp::common::components::types::GetOrbitingRadius (const double &e, const radian &a, const radian &v) |
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| glm::dvec3 | cqsp::common::components::types::MatrixConvertOrbParams (const double LAN, const double i, const double w, const glm::dvec3 &vec) |
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| glm::dvec3 | cqsp::common::components::types::ConvertOrbParams (const double LAN, const double i, const double w, const glm::dvec3 &vec) |
| | Transforms a vector to the orbital plane vector More...
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| glm::dvec3 | cqsp::common::components::types::ConvertToOrbitalVector (const double LAN, const double i, const double w, const double v, const glm::dvec3 &vec) |
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| Orbit | cqsp::common::components::types::Vec3ToOrbit (const glm::dvec3 &position, const glm::dvec3 &velocity, const double &GM, const double &time) |
| | Converts position and velocity to orbit. Note: you will have to set the reference body after the orbit is returned More...
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| double | cqsp::common::components::types::GetTrueAnomalyToAsymptope (const Orbit &orbit) |
| | Calculates v_inf, the true anomaly for the asymtope for a hyperbolic orbit The orbit is bouded within -v_inf < v < v_inf https://orbital-mechanics.space/the-orbit-equation/hyperbolic-trajectories.html#hyperbolic-trajectories-e-1. More...
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| glm::dvec3 | cqsp::common::components::types::OrbitToVec3 (const double &a, const double &e, const radian &i, const radian &LAN, const radian &w, const radian &v) |
| | Converts an orbit to a vec3. More...
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| double | cqsp::common::components::types::OrbitVelocity (const double v, const double e, const double a, const double GM) |
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| double | cqsp::common::components::types::AvgOrbitalVelocity (const Orbit &orb) |
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| glm::dvec3 | cqsp::common::components::types::OrbitVelocityToVec3 (const Orbit &orb, double v) |
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| glm::dvec3 | cqsp::common::components::types::OrbitVelocityToVec3 (const Orbit &orb) |
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| double | cqsp::common::components::types::SolveKeplerElliptic (const double &mean_anomaly, const double &ecc, const int steps=200) |
| | Computes eccentric anomaly for a elliptic or circular orbit (e < 1) in radians given mean anomaly and eccentricity More...
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| double | cqsp::common::components::types::SolveKeplerHyperbolic (const double &mean_anomaly, const double &ecc, const int steps=200) |
| | Computes eccentric anomaly for a hyperbolic or parabolic orbit (e > 1) in radians given mean anomaly and eccentricity More...
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| double | cqsp::common::components::types::EccentricAnomalyToTrueAnomaly (const double &ecc, const double &E) |
| | Calculates true anomaly from eccentricity and eccentric anomaly More...
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| double | cqsp::common::components::types::HyperbolicAnomalyToTrueAnomaly (const double &ecc, const double &H) |
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| double | cqsp::common::components::types::GetMtElliptic (const double &M0, const double &nu, const double &time, const double &epoch) |
| | Gets the Mean anomaly from the time More...
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| double | cqsp::common::components::types::GetMtHyperbolic (const double &M0, const double &nu, const double &time, const double &epoch) |
| | Calculate mean anomaly from time for a hyperbolic object More...
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| radian | cqsp::common::components::types::TrueAnomalyElliptic (const Orbit &orbit, const second &time) |
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| radian | cqsp::common::components::types::TrueAnomalyElliptic (const Orbit &orbit, const second &time, double &E_out) |
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| double | cqsp::common::components::types::GetCircularOrbitingVelocity (const double &GM, const double &radius) |
| | Get the circular orbiting velocity for the radius. More...
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| radian | cqsp::common::components::types::TrueAnomalyHyperbolic (const Orbit &orbit, const second &time) |
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| radian | cqsp::common::components::types::EccentricAnomaly (double v, double e) |
| | Calculates Eccentric anomaly More...
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| radian | cqsp::common::components::types::HyperbolicAnomaly (double v, double e) |
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| void | cqsp::common::components::types::UpdateOrbit (Orbit &orb, const second &time) |
| | Updates the orbit's true anomaly. More...
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| double | cqsp::common::components::types::GetTrueAnomaly (const Orbit &orb, const second &epoch) |
| | Get anomaly at epoch More...
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| glm::dvec3 | cqsp::common::components::types::CalculateVelocity (const double &E, const kilometer &r, const double &GM, const kilometer &a, const double &e) |
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| glm::dvec3 | cqsp::common::components::types::CalculateVelocityHyperbolic (const double &E, const double &r, const double &GM, const double &a, const double &e) |
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| glm::dvec3 | cqsp::common::components::types::CalculateVelocityElliptic (const double &E, const kilometer &r, const double &GM, const kilometer &a, const double &e) |
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| Orbit | cqsp::common::components::types::ApplyImpulse (const Orbit &orbit, const glm::dvec3 &impulse, double time) |
| | Applies impulse based on the vector impulse For some reason y is prograde, I'm not sure what the others are. TODO(EhWhoAmI): Determine the axis of thrust for each vector I think x is radial, and z is normal. More...
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| double | cqsp::common::components::types::OrbitVelocityAtR (const double GM, const double a, const double r) |
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| glm::dvec3 | cqsp::common::components::types::OrbitTimeToVec3 (const Orbit &orb, const second time) |
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| glm::dvec3 | cqsp::common::components::types::OrbitTimeToVelocityVec3 (const Orbit &orb, const second time) |
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| double | cqsp::common::components::types::CalculateTransferTime (const Orbit &orb1, const Orbit &orb2) |
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| double | cqsp::common::components::types::CalculateTransferAngle (const Orbit &start_orbit, const Orbit &end_orbit) |
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| double | cqsp::common::components::types::CalculatePhaseAngle (const Orbit &start_orbit, const Orbit &end_orbit, double epoch) |
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| double | cqsp::common::components::types::GetHyperbolicAsymptopeAnomaly (double eccentricity) |
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| double | cqsp::common::components::types::FlightPathAngle (double eccentricity, double v) |
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| glm::dvec3 | cqsp::common::components::types::GetOrbitNormal (const Orbit &orbit) |
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| double | cqsp::common::components::types::TrueAnomalyFromVector (const Orbit &orbit, const glm::dvec3 &vec) |
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| double | cqsp::common::components::types::AscendingTrueAnomaly (const Orbit &start, const Orbit &dest) |
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1.9.2