Variable attitude maneuver through tether for a ‘drifting’ twin satellite system in elliptic orbits-Reference-Cited by-同舟云学术

Variable attitude maneuver through tether for a ‘drifting’ twin satellite system in elliptic orbits

Published:1999-08 Issue:3 Volume:45 Page:135-142
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Kumar Krishna,Kumar K.D.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference11 articles.

1. Some aspects related to the satellite applications in non-stationary 24-hour orbits;Kumar;Acta Astronautica,1982

2. Kumar, K., Khosla, A. and Chaudhary, K. Tether as satellite attitude stabilizer in elliptic orbits: a novel concept, Paper No. AAS 93-735, presented at AAS/AIAA Astrodynamics Specialist Conference, Victoria, BC, Canada1993 and Advances in Astronautics, vol. 851994

3. Satellite attitude stabilization through tether;Kumar;Acta Astronautica,1995

4. Satellite attitude maneuver through tether: a novel concept;Kumar;Acta Astronautica,1997

5. Open-loop satellite librational control in elliptic orbits through tether;Kumar;Acta Astronautica,1997

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1. A review of space tether research;Progress in Aerospace Sciences;2008-01

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3. Line-of-sight-pointing for satellites in high altitude inclined elliptic orbits;IEEE Transactions on Aerospace and Electronic Systems;2005-07

4. An improved method of gravicraft propulsion;Acta Astronautica;2003-08

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