DVHohInc:

Path: Orbit/OrbitManeuver

% Compute impulses for an eccentric Hohmann transfer with a plane change.
 Transfers from periapsis of 1 to apoapsis of 2.
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   Form:
   [dv, dv1, dv2, Di1, Di2] = DVHohInc( e1, a1, e2, a2, Di, mu )
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   ------
   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

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   References: Hornbeck, R., Numerical Methods, Quantum, 1975, pp. 66-67.
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   See also: OptDIH, DVHohE, OrbMnvrInclAndHohm
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Children:

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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