Parameter Estimation-Based Fault Detection, Isolation and Recovery for Nonlinear Satellite Models

This brief is concerned with the problem of nonlinear fault detection, isolation, and recovery (FDIR) for the satellite's orbital and attitude models through construction of residual generators that are based on least-squares parameter estimation techniques. By viewing system anomalies caused by faults and/or malfunctions as changes of certain parameters in the system, our goal is to detect, isolate, and recover from faults through estimating these parameters and adaptively redesigning and reconfiguring the controllers. The convergence and robustness properties of the residual generators are analytically and experimentally investigated. Furthermore, the corresponding decision logic and thresholds for fault diagnosis are properly selected and specified. Numerical simulation results for the proposed technique as applied to nonlinear satellite models are presented to demonstrate its performance capabilities.

[1]  Rolf Isermann,et al.  Process fault detection based on modeling and estimation methods - A survey , 1984, Autom..

[2]  Bong Wie,et al.  Space Vehicle Dynamics and Control , 1998 .

[3]  A. Isidori Nonlinear Control Systems , 1985 .

[4]  Ron J. Patton,et al.  Robustness in Model-Based Fault Diagnosis: The 1995 Situation , 1995 .

[5]  Sai-Ming Li,et al.  Intelligent control of spacecraft in the presence of actuator failures , 1999, Proceedings of the 38th IEEE Conference on Decision and Control (Cat. No.99CH36304).

[6]  Richard Vernon Beard,et al.  Failure accomodation in linear systems through self-reorganization. , 1971 .

[7]  Jie Chen,et al.  Review of parity space approaches to fault diagnosis for aerospace systems , 1994 .

[8]  J. Kennedy National Aeronautics and Space Administration ROSAT , 2004 .

[9]  Paul M. Frank,et al.  Fault diagnosis in dynamic systems using analytical and knowledge-based redundancy: A survey and some new results , 1990, Autom..

[10]  James Lyke,et al.  Reconfigurable systems: A generalization of reconfigurable computational strategies for space systems , 2002, Proceedings, IEEE Aerospace Conference.

[11]  M. Massoumnia A geometric approach to the synthesis of failure detection filters , 1986 .

[12]  Ron J. Patton,et al.  Fault detection and diagnosis in aerospace systems using analytical redundancy , 1991 .

[13]  Alberto Isidori,et al.  Nonlinear control systems: an introduction (2nd ed.) , 1989 .

[14]  Alberto Isidori,et al.  A Geometric Approach to Nonlinear Fault Detection and Isolation , 2000 .

[15]  Chris J. Walter,et al.  Fault tolerant discovery and formation protocols for autonomous composition of spacecraft constellations , 2003, 2003 IEEE Aerospace Conference Proceedings (Cat. No.03TH8652).

[16]  Christopher Edwards,et al.  Sliding mode observers for robust detection and reconstruction of actuator and sensor faults , 2003 .

[17]  Jean-François Vandenrijt,et al.  Simulation and graphical representation of the orbit and the imaging parameter of Earth observation satellites , 2005 .

[18]  Anuradha M. Annaswamy,et al.  Robust Adaptive Control , 1984, 1984 American Control Conference.

[19]  Chee Pin Tan,et al.  Sliding mode observers for fault detection and isolation , 2002 .

[20]  Sai-Ming Li,et al.  On-line failure detection and identification (FDI) and adaptive reconfigurable control (ARC) in aerospace applications , 2001, Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148).

[21]  Rolf Isermann,et al.  Supervision, fault-detection and fault-diagnosis methods — An introduction , 1997 .

[22]  Harold Lee Jones,et al.  Failure detection in linear systems , 1973 .

[23]  Tao Jiang Nonlinear fault diagnosis and recovery for satellites using parameter estimation techniques , 2004 .

[24]  R. K. Mehra,et al.  Intelligent spacecraft control using multiple models, switching, and tuning , 1999, Proceedings of the 1999 IEEE International Symposium on Intelligent Control Intelligent Systems and Semiotics (Cat. No.99CH37014).