Results of flexible spacecraft attitude control studies utilizing hybrid coordinates
- 1 March 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (3), 264-273
- https://doi.org/10.2514/3.30258
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Influence of flexible appendages on dual-spin spacecraft dynamics and controlJournal of Spacecraft and Rockets, 1970
- Basic relations for control of flexible vehiclesAIAA Journal, 1970