Path: Orbit/OrbitManeuver
% Compute impulses for an eccentric Hohmann transfer with a plane change. Transfers from periapsis of 1 to apoapsis of 2. -------------------------------------------------------------------------- Form: [dv, dv1, dv2, Di1, Di2] = DVHohInc( e1, a1, e2, a2, Di, mu ) -------------------------------------------------------------------------- ------ Inputs ------ e1 Eccentricity of first orbit a1 Semi-major axis of first orbit e2 Eccentricity of final orbit a2 Semi-major axis of final orbit Di Change in inclination (rad) mu Gravitational parameter ------- Outputs ------- dv Total delta v dv1 Low orbit to transfer orbit delta v dv2 Transfer orbit to high orbit delta v Di1 Inclination correction during first Dv Di2 Inclination correction during second Dv -------------------------------------------------------------------------- References: Hornbeck, R., Numerical Methods, Quantum, 1975, pp. 66-67. -------------------------------------------------------------------------- See also: OptDIH, DVHohE, OrbMnvrInclAndHohm --------------------------------------------------------------------------
Orbit: OrbitCoord/A2Apogee Orbit: OrbitCoord/A2Perige Orbit: OrbitManeuver/OptDIH Common: General/DeBlankLT Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Linear/DupVect
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