Clohessy-Wiltshire M transformation matrix
M = CL_cw_Mmatrix(alt, delta_t [[, er, mu]])
Computes the Clohessy-Wiltshire M transformation matrix.
The local orbital reference frame tied to the target is LVLH (See CL_fr_lvlhMat).
Notes:
In the above formula:
- theta is equal to omega * delta_t, where omega is the target (= "reference") mean motion.
Target altitude (semi-major axis minus equatorial radius). [m] (1xN or 1x1)
Time step. [s] (1xN or 1x1)
(optional) Equatorial radius. Default: %CL_eqRad. [m] (1x1)
(optional) Gravitational constant. Default: %CL_mu. [m^3/s^2] (1x1)
Clohessy-Wiltshire "M" transformation matrix. (6x6xN)
CNES - DCT/SB
1) Mecanique spatiale, CNES - Cepadues 1995, Tome II, chapter 16