Path: Orbit/OrbitMechanics
% Computes the phase angles for a Hohmann intercept -------------------------------------------------------------------------- Form: [phi1, phi2] = PAHohmn( R1, R2, mu ) -------------------------------------------------------------------------- ------ Inputs ------ R1 Orbit radius 1 R2 Orbit radius 2 (target) mu Gravitational parameter ------- Outputs ------- phi1 phase angle between 1 and 2 at launch + implies 2 leads 1 phi2 phase angle between 1 and 2 at intercept + implies 1 leads 2 -------------------------------------------------------------------------- References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988, pp. 292-294. --------------------------------------------------------------------------
Orbit: OrbitMechanics/TTrnsHoh
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