Adaptive Fault-Tolerant Attitude Tracking Control for Flexible Spacecraft With Guaranteed Performance Bounds

Xiao, Yan; Ruiter, Anton de; Ye, Dong; Sun, Zhiyong

doi:10.1109/taes.2021.3123295

Cited by 29 publications

(10 citation statements)

References 50 publications

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“…As a key component of the active FTC, the fault detection and isolation (FDI) could increase the complexity of the FTC. To solve the above problems, some passive FTCs were proposed in [22], [49]- [51]. By combining the benefits of FLS and DO, the parametric uncertainties and fault components were resolved [22], [49].…”

Section: Introductionmentioning

confidence: 99%

Observer-Based Adaptive Fuzzy Finite-Time Attitude Control for Quadrotor UAVs

Liu,

Yang,

Wang

et al. 2023

IEEE Trans. Aerosp. Electron. Syst.

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Section: Introductionmentioning

confidence: 99%

Observer-Based Adaptive Fuzzy Finite-Time Attitude Control for Quadrotor UAVs

Liu,

Yang,

Wang

et al. 2023

IEEE Trans. Aerosp. Electron. Syst.

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“…It should be pointed out that the actuator fault problem is becoming more and more important with the growth of requirements for the satellite security. Some fault‐tolerant control (FTC) schemes have been proposed in References 23‐30 to guarantee closed‐loop system performance when the actuator faults occur. Notably, the problem of attitude tracking FTC was investigated in Reference 25 for a rigid spacecraft with actuator fault, actuator saturation and external disturbance.…”

Section: Introductionmentioning

confidence: 99%

Flexible performance‐based adaptive fault‐tolerant attitude tracking control for input‐constrained satellite

Li,

Yong,

Chen

et al. 2023

Adaptive Control & Signal

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SummaryUnder the actuator saturation and fault, the satellite attitude often violates the prescribed performance function, leading to the satellite attitude's instability. Therefore, the adaptive attitude tracking control problem for the satellite simultaneously considering the finite time‐based prescribed performance, the actuator saturation and the actuator fault is studied in this article. A modification performance function‐based control scheme is designed, which can avoid violating the designed modified performance functions when the actuator saturation occurs due to the actuator fault. A novel fault tolerant auxiliary system is developed, which is used to generate modification signals for adjusting the prescribed performance function. Consequently, the boundedness of all the closed‐loop signal under the designed control scheme is proved via Lyapunov function method. Finally, the feasibility of the designed satellite attitude control scheme is verified by a simulation example.

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“…Compared to a single spacecraft, the multi-spacecraft formation system can provide better reliability and higher observation accuracy for Earth observation and deep space exploration. [1][2][3][4][5][6][7] Specifically, by adjusting the relative positions between the members, the baseline length of the formation system could be changed to adapt to different space tasks. [8][9][10] Therefore, the formation reconfiguration control problem has aroused widespread concern recently.…”

Section: Introductionmentioning

confidence: 99%

Feasibility analysis and saturation control for underactuated spacecraft formation reconfiguration in elliptic orbits

Shao,

Zhou,

Xiao

et al. 2023

Proceedings of the Institution of Mechanical Engineers, Part G:

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This work proposes a saturation control scheme for underactuated spacecraft formation reconfiguration in elliptic orbits without radial or along-track thrust. Firstly, the rank criterion method is applied to analyze the controllability and feasibility of formation reconfiguration by linearizing the linear time-varying dynamics to linear time-invariant ones. Based on the inherent coupling of the linear time-varying system, the underactuated error dynamics are presented for either underactuated case. Subsequently, the developed underactuated saturation controller can ensure that the time-varying system trajectory asymptotically converges to the specified configuration. The Lyapunov-based analysis presents the constraint conditions of controller parameters and the stable reconfiguration accuracy of the system states. Finally, numerical simulations for both underactuated scenarios are performed in the environment with J2 perturbation to verify the validity of the proposed underactuated control scheme.

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Adaptive Fault-Tolerant Attitude Tracking Control for Flexible Spacecraft With Guaranteed Performance Bounds

Cited by 29 publications

References 50 publications

Observer-Based Adaptive Fuzzy Finite-Time Attitude Control for Quadrotor UAVs

Observer-Based Adaptive Fuzzy Finite-Time Attitude Control for Quadrotor UAVs

Flexible performance‐based adaptive fault‐tolerant attitude tracking control for input‐constrained satellite

Feasibility analysis and saturation control for underactuated spacecraft formation reconfiguration in elliptic orbits

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