An attitude control approach for compensation of satellite drift in elliptic synchronous orbits-Reference-Cited by-同舟云学术

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An attitude control approach for compensation of satellite drift in elliptic synchronous orbits

Published:1981-07 Issue:7 Volume:8 Page:719-731
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Kumar K.,Joshi V.K.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference13 articles.

1. Some applications of non-stationary geosynchronous orbits;Akin,1978

2. Stability of the planar librational motion of a satellite in an elliptic orbit;Brereton,1967

3. Mission design implications of an inclined elliptical geosynchronous orbit (International ultraviolet-explorer);Dial;J. Spacecraft and Rockets,1977

4. New solar attitude control approach for satellites in elliptic orbits;Joshi;J. Guidance and Control,1980

5. Solar pressure damping of satellite librations in elliptic orbits;Kumar;J. Astronaut. Sci.,1980

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Variable attitude maneuver through tether for a ‘drifting’ twin satellite system in elliptic orbits;Acta Astronautica;1999-08

2. Line-of-sight pointing stability for "drifting" satellites;IEEE Transactions on Aerospace and Electronic Systems;1999-04

3. Line-of-sight-pointing for drifting satellites at geostationary altitudes;Guidance, Navigation and Control Conference;1985-08-17

4. Some aspects related to the satellite applications in non-stationary 24-hour orbits;Acta Astronautica;1982-03

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