Attitude Tracking Control of Spacecraft with Reaction Wheel Disturbances Via Takagi-Sugeno Fuzzy Model

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Intelligent systems ; Volume 1 of 2
1. Verfasser: Si, Ying (VerfasserIn)
Weitere Verfasser: Ayoubi, Mohammad A. (VerfasserIn)
Pages:1
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2022
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