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TECHNICAL BRIEFS

Actuator Fault Estimation Scheme for Flight Applications

[+] Author and Article Information
Jiong-Sang Yee, Jian Liang Wang, Bin Jiang

School of Electrical and Electronic Engineering, Nanyang Technological University, Nanyang Ave., Singapore 639798

J. Dyn. Sys., Meas., Control 124(4), 701-704 (Dec 16, 2002) (4 pages) doi:10.1115/1.1515331 History: Received September 01, 2000; Revised May 01, 2002; Online December 16, 2002
Copyright © 2002 by ASME
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References

Chandler, P., and Wells, E., 1990, “Detection and Isolation of Control Element Failures on the NASA HIDEC F-15,” Proc. NAECON90, Dayton, OH.
Caglayan, A. K., Allen, S. M., and Wehmuller, K., 1988, “Evaluation of a Second Generation Reconfiguration Strategy for Aircraft Flight Control Systems Subjected to Actuator Failure/Surface Damage,” Proc. of National Aerospace and Electronics Conf., pp. 520–529.
Wu,  N. E., Zhang,  Y., and Zhou,  K., 2000, “Detection, Estimation and Accommodation of Loss of Control Effectiveness,” Int. J. Adapt. Control Signal Process., 14, pp. 775–795.
Theilliol, D., Noura, H., and Sauter, D., 1998, “Fault-Tolerant Control Method for Actuator and Component Faults,” Proc. Conf. on Decision and Control, pp. 604–609.
Boskovic, J. D., and Mehra, R. K., 1999, “Stable Multiple Model Adaptive Flight Control for Accommodation of a Large Class of Control Effector Failures,” Proc. of American Control Conf., pp. 1920–1924.
Narendra, K. S., and Annaswamy, A. M., 1989, Stable Adaptive Systems, Prentice Hall, Englewood, NJ.
Jiang,  B., Wang,  J. L., and Soh,  Y. C., “Robust Fault Diagnosis for a Class of Linear Systems with Uncertainty,” J. Guid. Control Dyn., 22(5), pp. 736–740.
Ackermann,  J., 1984, “Robustness Against Sensor Failures,” Automatica, 20(2), pp. 211–215.
Zhou, K., Doyle, J. C., and Glover, K., 1996, Robust Optimal Control, Prentice Hall, Englewood Cliffs, NJ.

Figures

Grahic Jump Location
Block diagram of fault-tolerant H flight control system design
Grahic Jump Location
Estimation of elevator effectiveness (solid: actual, dotted: estimate)
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C* output response (solid: command, dashed: response) based on nominal H flight controller
Grahic Jump Location
C* output response (solid: command, dashed: response) based on fault-tolerant H flight controller
Grahic Jump Location
Mixed-sensitivity formulation

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