Eliminating Secular Rotation of Spacecraft Orbits About the Angular Momentum Vector in J2 Perturbed Orbits
AIAA Guidance, Navigation and Control Conference and Exhibit
2008-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2008
|Springer Verlag | 2007
Eliminating Perigee Rotation in J2 Perturbed Orbits with a Constant Radial Acceleration AIAA Paper
British Library Conference Proceedings | 2007
|