Investigation on attitude disturbance control and vibration suppression for fuel-filled flexible spacecraft
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Computational Mechanics
Link
http://link.springer.com/content/pdf/10.1007/s10409-015-0431-8.pdf
Reference25 articles.
1. Banerjee, A.K., Pedreiro, N., Singhose, W.E.: Vibration reduction for flexible spacecraft following momentum dumping with/without slewing. J. Guid. Control Dyn. 24, 417–427 (2001)
2. Azadi, M., Fazelzadeh, S.A., Eghtesad, M., et al.: Vibration suppression and adaptive-robust control of a smart flexible satellite with three axes maneuvering. Acta Astronaut. 69, 307–322 (2011)
3. Hu, Q., Ma, G.: Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver. Aerosp. Sci. Technol. 9, 307–317 (2005)
4. Azadi, E., Eghtesad, M., Fazelzadeh, S.A., et al.: Vibration suppression of smart nonlinear flexible appendages of a rotating satellite by using hybrid adaptive sliding mode/Lyapunov control. J. Vib. Control 19, 975–991 (2013)
5. Hu, Q., Xiao, B.: Robust adaptive backstepping attitude stabilization and vibration reduction of flexible spacecraft subject to actuator saturation. J. Vib. Control 17, 1657–1671 (2011)
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