Path: AerospaceUtils/Coord
-------------------------------------------------------------------------- Generate the quaternion that transforms from the ECI to the Hills frame. The coordinates of the Hills frame are defined as: x: Radial z: Orbit-normal, or cross-track y: Completes RHS (Along-track for circular orbits) The relative position vector in the Frenet frame can be computed as: rF = QForm( qEF, drE ); where dr is the relative position vector in the ECI frame. Or you may obtain the transformation matrix, mEF, as the second output. In this case, use: rF = mEF*drE; -------------------------------------------------------------------------- Usages: qEH = QHills( rE, vE ); [qEH,mEH] = QHills( rE, vE ); -------------------------------------------------------------------------- ------ Inputs ------ rE (3,n) Position vectors vE (3,n) Velocity vectors ------- Outputs ------- q (4,n) Quaternions --------------------------------------------------------------------------
Common: Graphics/Plot2D Common: Quaternion/Mat2Q Math: Linear/Cross Math: Linear/Unit
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