Path: Orbit/OrbitManeuver
% Delta-V for a Hohmann transfer between circular non coplanar orbits.
The delta-Vs are at
The initial orbit
The final orbit
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Form:
[deltaV, deltaI, tOF] = OrbMnvrInclAndHohm( rI, rF, iI, iF, mu )
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Inputs
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rI (1,1) Initial radius
rF (1,1) Final radius
II (1,1) Initial inclination (rad)
iF (1,1) Final inclination (rad)
mu (1,1) Gravitational parameter
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Outputs
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deltaV (.) Delta-V data structure.
.total (1,1) Total required delta-V
.a (1,1) Delta-V at point a
.b (1,1) Delta-V at point b
deltaI (.) Delta-Inclination data structure.
.total (1,1) Total required delta-Inc (rad)
.a (1,1) Delta-Inclination at point a (rad)
.b (1,1) Delta-Inclination at point b (rad)
tOF (.) Time of flight
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Reference: Vallado, D. A. (1997.) Fundamentals of Astrodynamics and
Applications. pp 281-282.
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