Nutation damping and vibration isolation in a flexibly coupled dual-spin spacecraft
- 1 August 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (8), 817-823
- https://doi.org/10.2514/3.30327
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- TACSAT I nutation dynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Attitude stability criteria for dual spin spacecraft.Journal of Spacecraft and Rockets, 1967
- Nutational stability of an axisymmetric body containing a rotorJournal of Spacecraft and Rockets, 1964