Path: FormationFlying/Transformation
% Compute a Hills state from a relative ECI state This function takes the absolute position and velocity in the ECI frame along with the relative position and velocity in the ECI frame, and computes the relative position and velocity in the curvilinear Hill's frame. -------------------------------------------------------------------------- Form: [rH,vH] = AbsRelECI2Hills( r0, v0, dr, dv ); -------------------------------------------------------------------------- ------ Inputs ------ r0 (3,1) Reference position in ECI frame r0 (3,1) Reference velocity in ECI frame dr (3,n) Relative position in ECI frame dv (3,n) Relative velocity in ECI frame ------- Outputs ------- rH (3,n) Curvilinear Hills frame position [dR; r1*dTheta; dZ ] vH (3,n) Curvilinear Hills frame velocity [dRDot; r1*dThetaDot + r1Dot*dTheta; dZDot] --------------------------------------------------------------------------
FormationFlying: Coord/GetHillsMats SC: BasicOrbit/E2M SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/RV2El Common: CommonData/SwooshWatermark Common: General/CellToMat 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
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