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Adaptive Compensation of Aircraft Actuation Failures Using an Engine Differential Model

Adaptive Compensation of Aircraft Actuation Failures Using an Engine Differential Model,10.1109/TCST.2007.906273,IEEE Transactions on Control Systems

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Adaptive Compensation of Aircraft Actuation Failures Using an Engine Differential Model   (Citations: 5)
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This paper investigates actuator failure compensation for aircraft flight control in a novel framework. A general failure compensation scheme for asymptotic tracking is developed based on a direct adaptive control approach. This control scheme is capable of utilizing the remaining control authority to achieve the desired performance in the presence of unknown and uncertain constant actuator failures occurring at unknown time instants. A nonlinear aircraft model that incorporates independently adjustable engine throttles and ailerons is employed and linearized to describe the aircraft's longitudinal and lateral motion. This model captures the key features of aircraft flight dynamics when in the engine differential mode. The proposed control scheme is applied to a transport aircraft model in the presence of three types of failures during operation: rudder failure, aileron failure, and engine malfunction. Simulation results are presented to assess the effectiveness of this adaptive failure compensation design.
Journal: IEEE Transactions on Control Systems Technology - IEEE TRANS CONTROL SYST TECHN , vol. 16, no. 5, pp. 971-982, 2008
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    • ...The existing fault-tolerant design approaches for aircraft can be broadly classified into two groups, namely the passive approach (Veillette, Medanic, and Perkins 1992; Zhao and Jiang 1998; Yang, Wang, and Soh 2001; Liao, Wang, and Yang 2002; Yang and Lum 2003; Cheng and Zhao 2004; Feng, Wang, Poh, and Liao 2005; Wu and Zhang 2006) and the active approach (Wang and Daley 1996; Bodson and Groszkiewicz 1997; Boskovic and Mehra 1999, 2001; Chen and Patton 1999; Tao, Joshi, and Ma 2001; Zhang and Jiang 2002; Tang, Tao, and Wang 2004; Wang, Huang, and Tan 2004; Zhang, Wang, Hesketh, Clements, and Eaton 2005; Jiang, Staroswiecki, and Cocquempot 2006; Belkharraz and Sobel 2007; Tang, Tao, and Joshi 2007; Chen and Chowdhury 2008; Liu, Tang, Tao, and Joshi 2008; Jin and Yang 2009; Zhang, Jiang, and Shi 2009, 2010; Yang and Ye 2010)...

    Xiao-Zheng Jin, et al. Robust H∞ and adaptive tracking control against actuator faults with a...

    • ...There are several possible avenues in adaptive control of linear systems with actuator failures recently, for example, direct adaptive control [8,18,19], linear matrix inequality (LMI) technique [22,23], multiple model design [1–3,9], neural network-based design [24], etc...

    Zhengqiang Zhang, et al. Adaptive output feedback control of nonlinear systems with actuator fa...

    • ...Using small perturbation linearization [7], [10], we can obtain the linearized aircraft model with the following structure:...

    Yu Liu, et al. Multivariable MRAC for aircraft with abrupt damages

    • ...The linearization of the aircraft model under asymmetric damages is preformed following the same procedure of small perturbation linearization used in [8]...

    Yu Liu, et al. Multivariable MRAC using Nussbaum gains for aircraft with abrupt damag...

    • ...Similar to that in [8], the coupling terms are determined by the nominal settings of certain actuators at the specified equilibrium...
    • ...Stability analysis. To verify the desired stability and tracking properties, we choose a piecewise continuous Lyapunov function similar to those in [8], [11]...

    Yu Liu, et al. Modeling and multivariable adaptive control of aircraft with synthetic...

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