The DOI matches its Crossref record; 2 of the 2 references it cites were found in a registry or an index.
Adaptive Sliding Mode Fault Tolerant Attitude Tracking Control for Flexible Spacecraft Under Actuator Saturation
Abstract
A novel fault tolerant attitude tracking control scheme is developed for flexible spacecraft with partial loss of actuator effectiveness fault. Neural networks are first introduced to account for system uncertainties, and an adaptive sliding mode controller is derived by using on-line updating law to estimate the bound of actuator fault such that any information of the fault is not required. To further address actuator saturation problem, a modified fault tolerant control law is then presented to ensure that the resulting control signal will never incur saturation. It is shown that the roll, pitch and yaw angle trajectories can globally asymptotically track the desired attitude in the face of faulty actuator, system uncertainties, external disturbances and even actuator saturation. A simulation example of a flexible spacecraft is given to illustrate the effectiveness of the proposed controller.
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Citations
Cites
Bibliographical review on reconfigurable fault-tolerant control systems
Zhang, Y., & Jiang, J. (2008) · Annual Reviews in Control · doi:10.1016/j.arcontrol.2008.03.008 · Cited by 2,652
Self-citationFault-tolerant Flight Control and Guidance Systems
Ducard, G. J. J. (2009) · Advances in Industrial Control · doi:10.1007/978-1-84882-561-1 · Cited by 337
Cited by
Van, M., Mavrovouniotis, M., & Ge, S. S. (2019) · IEEE Transactions on Systems, Man, and Cybernetics: Systems · doi:10.1109/tsmc.2017.2782246 · Cited by 478
Fault-Tolerant Attitude Stabilization for Satellites Without Rate Sensor
Xiao, B., Huo, M., Yang, X., & Zhang, Y. (2015) · IEEE Transactions on Industrial Electronics · doi:10.1109/tie.2015.2432107 · Cited by 99
Self-citationZheng, M., Wu, Y., & Li, C. (2021) · Aerospace Science and Technology · doi:10.1016/j.ast.2021.107126 · Cited by 37
Metadata
- Authors
- Xiao, B., Hu, Q., & Zhang, Y.
- Venue
- IEEE Transactions on Control Systems Technology
- Published
- 2012-11
- Volume
- 20
- Issue
- 6
- Pages
- 1605-1612
- ISSN
- 1063-6536 (ISSN-L)
- 1558-0865
- OpenAlex
- W2075841074
- Cited by
- 451
- References
- 2
- FWCI
- 29.21
- Type
- journal article
- Language
- en
- Open access
- closed
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- CoChat. (2026). Citation check: Adaptive Sliding Mode Fault Tolerant Attitude Tracking Control for Flexible Spacecraft Under Actuator Saturation. https://app.cochat.ai/papers/10.1109/tcst.2011.2169796
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- Xiao, B., Hu, Q., & Zhang, Y. (2012). Adaptive Sliding Mode Fault Tolerant Attitude Tracking Control for Flexible Spacecraft Under Actuator Saturation. IEEE Transactions on Control Systems Technology. https://doi.org/10.1109/tcst.2011.2169796
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