Path: FormationFlying/Transformation
% Convert element differences to eccentric geometric goals.
Since version 7.
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Usage:
g = FFEccDeltaElem2Goals( el0, dEl, type );
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Inputs
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el0 (1,6) Initial reference orbital elements
dEl (1,6) Initial orbital element differences
type (1) Element set type
- 1 [a,theta,i,q1,q2,W] (Alfriend format)
- 2 [a,i,W,w,e,M] (standard format)
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Outputs
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g (.) Geometric goals data structure
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AC: ACData/ACTConstants FormationFlying: Coord/GetHillsMats FormationFlying: EccDynamics/FFEccDH FormationFlying: EccDynamics/FFEccGoals FormationFlying: EccDynamics/FFEccProp FormationFlying: EccDynamics/FFEccRMat FormationFlying: EccDynamics/FFEccXExt FormationFlying: EccDynamics/FFEccYExt FormationFlying: EccDynamics/FFEccZExt EccDynamics: Derivatives/FFEccDDX EccDynamics: Derivatives/FFEccDDY EccDynamics: Derivatives/FFEccDDZ EccDynamics: Derivatives/FFEccDX EccDynamics: Derivatives/FFEccDY EccDynamics: Derivatives/FFEccDZ FormationFlying: Transformation/ECI2Hills FormationFlying: Transformation/FFEccDeltaElem2Hills FormationFlying: Transformation/FFEccHills2Goals FormationFlying: Utility/NuDot FormationFlying: Utility/Time2NuDomain FormationFlying: Visual/FFEccAnalyzeShape Orbit: OrbitCoord/Alfriend2El SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/OrbRate SC: BasicOrbit/RV2El SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Solvers/NewtRaph Math: Trigonometry/WrapPhase
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