Real-Time Identification of Aircraft Physical Models for Fault Tolerant Flight Control

Author:

Chu Ping,Mulder Jan Albert (Bob),Breeman Jan

Publisher

Springer Berlin Heidelberg

Reference36 articles.

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2. Breeman, J.H., Erkelens, L.J.J., Nieuwpoort, A.M.H.: Determination of performance and stability characteristics from dynamic manoeuvres with a transport aircraft using parameter identification. In: AGARD FMP Symposium on Flight Test Techniques, Lisbon (1984)

3. Breeman, J.H., Simons, J.L.: Evaluation of a method to extract performance data from dynamic manoeuvres for a jet transport aircraft. In: 11th ICAS congress, Lisbon (1978)

4. Chu, Q.P., Mulder, J.A., Sridhar, J.K.: Analytical and numerical comparison of the maximum likelihood method and two step method for aircraft state and parameter estimation. In: Proceedings of the 10th IFAC Symposium on System Identification, SYSID 1994, July 1994, vol. 3, pp. 61–66 (1994)

5. Chu, Q.P., Mulder, J.A., Van Woerkom, P.T.L.M.: Aircraft flight path reconstruction with nonlinear adaptive filters. In: Proceedings of the American Control Conference, ACC, Seattle, vol. 2, pp. 1196–1200 (1995)

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