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Fault mode probability factor based fault-tolerant control for dissimilar redundant actuation system

Chinese Journal of Aeronautics 2018年第5期31卷 965-975页

作者： Jun WANG Shaoping WANG Xingjian WANG Mileta M.TOMOVIC Cun SHI School of Automation Science and Electrical Engineering Beihang University College of Engineering and Technology Old Dominion University

This paper presents a Fault Mode Probability Factor（FMPF） based Fault-Tolerant Control（FTC） strategy for multiple faults of dissimilar redundant actuation system（DRAS）composed of Hydraulic Actuator（HA） and Electro-Hydrostatic Actuator（EHA）. The long-term service and severe working conditions can result in multiple gradual faults which can ultimately degrade the system performance, resulting in the system model drift into the fault state characterized with parameter uncertainty. The paper proposes to address this problem by using the historical statistics of the multiple gradual faults and the proposed FMPF to amend the system model with parameter uncertainty. To balance the system model precision and computation time, a Moving Window（MW） method is used to determine the applied historical statistics. The FMPF based FTC strategy is developed for the amended system model where the system estimation and Linear Quadratic Regulator（LQR） are updated at the end of system sampling period. The simulations of DRAS system subjected to multiple faults have been performed and the results indicate the effectiveness of the proposed approach.

关键词： dissimilar redundant actuation system Fault mode probability factor Fault-tolerant control Linear quadratic regulator Monte Carlo simulation Moving window

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Active fault tolerant control for vertical tail damaged aircraft with dissimilar redundant actuation system

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Chinese Journal of Aeronautics 2016年第5期29卷 1313-1325页

作者： Wang Jun Wang Shaoping Wang Xingjian Shi Cun Mileta M.Tomovic School of Automation Science and Electrical Engineering Beihang University College of Engineering and Technology Old Dominion University

This paper proposes an active fault-tolerant control strategy for an aircraft with dissimilar redundant actuation system （DRAS） that has suffered from vertical tail damage. A damage degree coefficient based on the effective vertical tail area is introduced to parameterize the damaged flight dynamic model. The nonlinear relationship between the damage degree coefficient and the corresponding stability derivatives is considered. Furthermore, the performance degradation of new input channel with electro-hydrostatic actuator （EHA） is also taken into account in the damaged flight dynamic model. Based on the accurate damaged flight dynamic model, a composite method of linear quadratic regulator （LQR） integrating model reference adaptive control （MRAC） is proposed to reconfigure the fault-tolerant control law. The numerical simulation results validate the effectiveness of the proposed fault-tolerant control strategy with accurate flight dynamic model. The results also indicate that aircraft with DRAS has better fault-tolerant control ability than the traditional ones when the vertical tail suffers from serious damage.

关键词： dissimilar redundant actuation system Electro-hydrostatic actuator Fault-tolerant control Linear quadratic regulator Model reference adaptivecontrol Nonlinear aircraft model Vertical tail loss

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