Deadbeat Nutation Controller for Momentum Bias Stabilized Spacecraft
- 1 July 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
- Vol. 3 (4) , 361-368
- https://doi.org/10.2514/3.56002
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Attitude Stability of a Pseudorate Jet-Controlled Flexible SpacecraftJournal of Guidance and Control, 1979
- Gyro-based attitude reference systems for communications satellitesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- High pointing accuracy with a momentum bias attitude control systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Pseudorate sawtooth-pulse-reset control system analysis and design.Journal of Spacecraft and Rockets, 1967