Three-Dimensional Response Characteristics for Spacecraft with Deploying Flexible Appendages
- 1 September 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
- Vol. 4 (5) , 650-656
- https://doi.org/10.2514/3.56123
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Two Decades of Spacecraft Attitude ControlJournal of Guidance and Control, 1979
- First Steps into Space, 1946-1978Journal of Spacecraft and Rockets, 1979
- Strapdown Navigation Technology: A Literature SurveyJournal of Guidance and Control, 1978
- Attitude Dynamics of Satellites with Flexible Appendages- A Brief ReviewJournal of Spacecraft and Rockets, 1974
- On the dynamics of an axially moving beamJournal of the Franklin Institute, 1974