DYNAMlC STABILITY OF A GRAVITY GRADIENT STABILIZED SATELLITE HAVING LONG FLEXIBLE ANTENNAS-Reference-Cited by-同舟云学术

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DYNAMlC STABILITY OF A GRAVITY GRADIENT STABILIZED SATELLITE HAVING LONG FLEXIBLE ANTENNAS

Published:1966-08-15 Issue: Volume: Page:
ISSN:
Container-title:Guidance and Control Conference
language:
Short-container-title:

Author:

DOW P.¹,SCAMMELL F.¹,MURRAY F.¹,CARLSON N.¹,BUCK I.¹

Affiliation:

1. AVCO SPACE SYSTEMS DIVISION, LOWELL, MA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1966-1826

Reference20 articles.

1. May 1965;Buxton A. C.

2. Katucki, R. J., and Moyer, R. G. "System Analysis and Design of a Class of Gravity Gradient Satellites Utilizing Viscous Coupling between the Earth's Magnetic Field and Gravity Gradient Fields, If presented at the Symposium on Passive Gravity Gradient Stabilization, NASA Ames (May 1965).

Cited by 10 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. Transient dynamics during the orbiter based deployment of flexible members;22nd Aerospace Sciences Meeting;1984-01-09

2. Attitude dynamics of a satellite during deployment of large plate-type structures;22nd Structures, Structural Dynamics and Materials Conference;1981-04-06

3. Attitude Dynamics of Satellites with Flexible Appendages- A Brief Review;Journal of Spacecraft and Rockets;1974-11

4. Liapunov stability analysis of spinning flexible spacecraft.;AIAA Journal;1973-04

5. Optimization of RAE satellite boom deployment timing;Journal of Spacecraft and Rockets;1970-09

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