Abstract
In this study we consider some further aspects of a velocity-free control scheme for regulating the attitude of a rigid spacecraft with gas jet and momentum exchange actuators. In particular, we consider some structural properties of the proposed controller that ensure asymptotic stability of the required attitude set-point. As shown, these properties are useful for studying stability when time-delay appears in the feedback loop.
| Original language | English |
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| Pages | 799-804 |
| Number of pages | 6 |
| State | Published - 1 Dec 2001 |
| Event | Proceedings of the 2001 IEEE International Conference on Control Applications CCA '01 - Mexico City, Mexico Duration: 5 Sep 2001 → 7 Sep 2001 |
Conference
| Conference | Proceedings of the 2001 IEEE International Conference on Control Applications CCA '01 |
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| Country/Territory | Mexico |
| City | Mexico City |
| Period | 5/09/01 → 7/09/01 |
Keywords
- Attitude regulation
- Gas-jet actuators
- Momentum exchange actuators
- Spacecraft
- Time-delay
- Velocity-free controllers
ASJC Scopus subject areas
- Control and Systems Engineering