Code covered by the BSD License
- atan3 (a, b)
four quadrant inverse tangent
- eci2orb1 (mu, r, v)
convert eci state vector to six classical orbital
- oeprint1(mu, oev)
print six classical orbital elements
- om_constants
astrodynamic and utility constants
- orb2eci(mu, oev)
convert classical orbital elements to eci state vector
- pvector (ri, vi, x)
primer vector and derivative magnitudes
- pviniz (tof, r1, v1, dv1,...primer vector initialization
- stm2 (mu, tau, ri, vi)
two body state transition matrix
- svprint(r, v)
print position and velocity vectors and magnitudes
- twobody2 (mu, tau, ri, vi)solve the two body initial value problem
- phasing.m
-
View all files
Two Impulse Phasing Analysis
by David Eagle
30 Nov 2012
(Updated 22 Jul 2013)
Phasing analysis between two coplanar circular orbits using a two impulse Hohmann transfer.
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| File Information |
| Description |
PDF document and a MATLAB script called phasing.m that performs a phasing or rendezvous analysis accomplished with a two impulse, coplanar Hohmann transfer. This script computes and displays a complete analysis of the phasing maneuvers along with a graphics display of the initial orbit and final orbits, the transfer trajectory and the orbital locations of the spacecraft and maneuvers. |
| MATLAB release |
MATLAB 7.14 (R2012a)
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| Updates |
| 22 Jul 2013 |
Added ideal transfer angle example to PDF document. |
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