Orbital Mechanics
Orbital Mechanics
Orbital Mechanics
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Sample Plane Change Maneuver<br />
Delta V (km/sec)<br />
7<br />
6<br />
5<br />
4<br />
3<br />
2<br />
1<br />
0<br />
0 10 20 30<br />
Initial Inclination Change (deg)<br />
Optimum initial plane change = 2.20°<br />
DV1<br />
DV2<br />
DVtot<br />
<strong>Orbital</strong> <strong>Mechanics</strong><br />
Principles of Space Systems Design