Variable Attitude Compensation Through Tether for Comsats Geosynchronous Orbits in Drifting/Inclined
Krishna Kumar, K. D. Kumar
Journal of Spacecraft and Rockets ; 37 , 2 ; 290-293
2000
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Variable attitude maneuver through tether for a 'drifting' twin satellite system in elliptic orbits
Online Contents | 1999
|Inclined and eccentric geosynchronous satellite orbits
AIAA | 1982
|Online Contents | 1998
|