Hohmann transfer - DEPRECATED
[delta_v,dv1,dv2,anv1,anv2] = CL_man_hohmann(ai,af [,mu])
This function is deprecated.
Replacement function: CL_man_dvHohmann
Computes the maneuvers of a Hohmann transfer from an initial circular orbit with semi major axis ai to a final circular orbit with semi major axis af.
The output argument delta_v is the sum of the norms of the velocity increments required (|dv1| + |dv2|).
Velocity increments are expressed in spherical coordinates in the "qsw" frame.
Semi-major axis of initial circular orbit. [m] (1xN or 1x1)
Semi-major axis of final circular orbit. [m] (1xN or 1x1)
(optional) Gravitational constant. [m^3/s^2] (default value is %CL_mu)
Total delta-v required = |dv1| + |dv2|. [m/s] (1xN)
First velocity increment, in spherical coordinates in the "qsw" local orbital frame [lambda;phi;|dv|] [rad,rad,m/s]. (3xN)
Second velocity increment, in spherical coordinates in the "qsw" local orbital frame [lambda;phi;|dv|]. [rad,rad,m/s] (3xN)
True anomaly at the location of the first velocity increment (in the initial orbit): as the initial orbit is circular, anv1 is arbitrary. (1xN)
True anomaly at the location of the second velocity increment (in the intermediate orbit). [rad] (1xN)
CNES - DCT/SB