\(H_\infty\) control for flexible spacecraft with time-varying input delay
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Publication:474677
DOI10.1155/2013/839108zbMath1299.93208OpenAlexW1999737479WikidataQ59030567 ScholiaQ59030567MaRDI QIDQ474677
Publication date: 24 November 2014
Published in: Mathematical Problems in Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1155/2013/839108
Related Items (2)
Global attitude stabilization of rigid spacecraft with unknown input delay ⋮ Composite fault tolerant attitude control for flexible satellite system under disturbance and input delay
Cites Work
- An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts
- Adaptive robust tracking for flexible spacecraft in presence of disturbances
- Robust H(infinity) control design for the Space Station with structured parameter uncertainty
- H-infinity control of an Earth observation satellite
- Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver
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