Computer aided design of failure detection and identification and adaptive reconfigurable control systems for aerospace applications

The paper describes a systematic computer-aided design procedure for failure detection and identification (FDI) and adaptive reconfigurable control (ARC) for aerospace applications. The overall approach is based on a decentralized FDI-ARC scheme integrating separate modules for sensor, control effector and engine FDI with that for structural damage FDI. One of the important issues in this context is information exchange among the modules. In the paper we focus on the module for FDI-ARC in the presence of control effector failures, and describe our approach as well as future work in this area.

[1]  M. B. Subrahmanyam.  H∞ Design of the F/A-18A Automatic Carrier Landing System , 1995 .

[2]  Manfred Morari,et al.  State-space interpretation of model predictive control , 1994, Autom..

[3]  Y. Bar-Shalom,et al.  The interacting multiple model algorithm for systems with Markovian switching coefficients , 1988 .

[4]  M. B. Subrahmanyam,et al.  H-infinity design of F/A-18A automatic Carrier Landing System , 1994 .

[5]  Jovan D. Boskovic,et al.  Stable multiple model adaptive flight control for accommodation of a large class of control effector failures , 1999, Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251).

[6]  Raman K. Mehra,et al.  Intelligent adaptive control of a tailless advanced fighter aircraft (TAFA) in the presence of wing damage , 1999 .

[7]  Kumpati S. Narendra,et al.  Adaptive control using multiple models , 1997, IEEE Trans. Autom. Control..

[8]  Manfred Morari,et al.  Model predictive control: Theory and practice - A survey , 1989, Autom..

[9]  Jovan D. Boskovic.  A multiple model-based controller for nonlinearly-parametrized plants , 1997, Proceedings of the 1997 American Control Conference (Cat. No.97CH36041).

[10]  G. Gattu,et al.  Nonlinear Quadratic Dynamic Matrix Control with State Estimation , 1992 .

[11]  Raman K. Mehra,et al.  Failure detection and identification and fault tolerant control using the IMM-KF with applications to the Eagle-Eye UAV , 1998, Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No.98CH36171).

[12]  C. R. Cutler,et al.  Dynamic matrix control¿A computer control algorithm , 1979 .

[13]  Jovan D. Boskovic,et al.  A multiple model predictive scheme for fault-tolerant flight control design , 1998, Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No.98CH36171).

[14]  J. Richalet,et al.  Industrial applications of model based predictive control , 1993, Autom..

[15]  Youmin Zhang,et al.  Detection and diagnosis of sensor and actuator failures using IMM estimator , 1998 .

[16]  Kumpati S. Narendra,et al.  Adaptation and learning using multiple models, switching, and tuning , 1995 .