Sensitivity Discriminating Observer Design for Instrument Failure Detection

IEEE Transactions on Aerospace and Electronic Systems

Volumn AES-16, Issue 4, 1980, Pages 460-467

  Frank, P M ^a   Keller, L ^a  

^a UNIVERSITY OF DUISBURG ESSEN   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

REDUNDANCY;

EID: 0019038474     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.1980.308975     Document Type: Article

References (7)

1. A.S. Willsky “A survey of design methods for failure detection in dynamic systems.” Automatica, vol. 12, pp. 601–611, 1976.
2. R.C. Montgomery and A.K. Caglayan “Failure accommodation in digital flight control systems by Bayesian decision theory,” J Aircraft, vol. 13, pp. 69–75, Feb. 1976.
3. R.V. Beard, “Failure accommodation in linear systems through self-reorganization,” Man Vehicle Lab., Cambridge, Mass., Rep. MVT-71-1, Feb. 1971.
4. H.L. Jones, “Failure detection in linear systems,” Ph.D. dissertation, Dep. Aeronautics and Astronautics, M.I.T., Cambridge, Mass., Sept. 1973.
5. A.S. Willsky, J.J. Deyst, Jr., and B.S. Crawford, “Adaptive filtering and self-test methods for failure detection and compensation,” Proc. 1974 Joint Automatic Control Conf, Austin, Tex., pp. 637–645.
6. T.B. Cunningham, G.L. Hartmann, R.D. Poyneer, R. Hendrick, D.N. Carlson, D. Shaner, and G. Stein, “Fault tolerant digital flight control with analytical redundancy,” Air Force Flight Dynamics Lab., Tech Rep. AFFDL-TR-77-25, May 1977.
7. R.N. Clark, D.C. Fosth and V.M. Walton “Detecting instrument malfunctions in control systems,” IEEE Trans. Aerosp. Electron. Syst., vol. AES-11, pp. 465–473, July 1975.