Code covered by the BSD License
- atan3 (a, b)
four quadrant inverse tangent
- brent (f, x1, x2, rtol)
solve for a single real root of a nonlinear equation
- eci2orb1 (mu, r, v)
convert eci state vector to six classical orbital
- hohmfunc (x)
inclination objective function
- 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
- hohmann.m
-
View all files
The Hohmann Orbit Transfer
by David Eagle
06 Nov 2012
(Updated 12 Jul 2013)
Computes characteristics for coplanar and non-coplanar Hohmann transfers.
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| File Information |
| Description |
PDF document and MATLAB script for computing the delta-v and orbit transfer characteristics between two coplanar or non-coplanar circular orbits. |
| MATLAB release |
MATLAB 7.14 (R2012a)
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| Updates |
| 08 Jul 2013 |
Added three-dimensional graphic display of solution. Graphic display includes initial, transfer and final orbits. |
| 12 Jul 2013 |
Added primer vector graphics. Updated PDF document. |
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