Influence of flexible appendages on dual-spin spacecraft dynamics and control
- 1 September 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 7 (9), 1049-1056
- https://doi.org/10.2514/3.30101
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Effects of energy dissipation on the attitude stability of dual-spinsatellites.AIAA Journal, 1969
- Use of synthetic modes in hybrid coordinate dynamic analysis.AIAA Journal, 1968
- Attitude stability criteria for dual spin spacecraft.Journal of Spacecraft and Rockets, 1967
- Modal method for analysis of free rotations of spacecraft.AIAA Journal, 1967
- Observations on the dynamic behavior of large flexible bodies in orbit.AIAA Journal, 1967
- Rotation of Artificial Earth SatellitesNature, 1958