An observer-based adaptive fault-tolerant control for hypersonic vehicle with unexpected centroid shift and input
1School of Science, Jiangsu University of Science and Technology, Zhenjiang 212000, China.
This study presents a fault-tolerant control (FTC) scheme for hypersonic reentry vehicles (HSVs) facing actuator failures and center-of-mass shifts. The adaptive FTC ensures stable attitude control despite uncertainties and constraints.
Area of Science:
- Aerospace Engineering
- Control Systems Theory
Background:
- Hypersonic reentry vehicles (HSVs) face complex control challenges due to actuator failures and dynamic shifts.
- Unexpected center-of-mass movement introduces coupled uncertainties like varying inertia and eccentric torque, complicating control design.
Purpose of the Study:
- To develop an adaptive fault-tolerant control (FTC) strategy for HSVs.
- To address challenges posed by actuator failures, input constraints, and unknown center-of-mass shifts.
Main Methods:
- An adaptive observer combining fault and sliding-mode observers estimates system uncertainties.
- An adaptive FTC scheme utilizes estimated states, adaptive backstepping control, and auxiliary compensation for input saturation.
- Lyapunov stability theory ensures convergence and boundedness of closed-loop signals.
Main Results:
- The proposed FTC scheme effectively handles unknown system uncertainties and actuator failures.
- The adaptive observer successfully estimates detrimental unknown effects caused by centroid shifts.
- Simulation results validate the controller's effectiveness in maintaining attitude stability.
Conclusions:
- The developed adaptive FTC scheme provides robust control for HSVs under adverse conditions.
- The innovative observer design overcomes challenges associated with singular matrices due to centroid shifts.
- The approach ensures attitude tracking error convergence and overall system stability.
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