System identification and stability evaluation of an unmanned aerial vehicle from automated flight tests-Reference-Cited by-同舟云学术

System identification and stability evaluation of an unmanned aerial vehicle from automated flight tests

Published:2003-05 Issue:5 Volume:17 Page:654-667
ISSN:1226-4865
Container-title:KSME International Journal
language:en
Short-container-title:KSME International Journal

Author:

Suk Jinyoung,Lee Younsaeng,Kim Seungjoo,Koo Hueonjoon,Kim Jongseong

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF02983861.pdf

Reference22 articles.

1. Gelb, A., 1974,Applied Optimal Estimation, MIT Press, Cambridge, MA.

2. Harael, P. and Jategaonkar, R., 1996, “Evolution of Flight Vehicle System Identification,”Journal of Aircraft, Vol. 33. No. 1, pp. 9–28.

3. Hoak, D., 1972USAF Stability and Control DATCOM, Flight Control Division, Air Force Flight Dynamics Laboratory, Wright-Peterson Air Force Base, Ohio.

4. Iliff, K. and Maine, R., 1984,More Than You May Want To Know About Maximum Likelihood Estimation, NASA-TM-85905.

5. Iliff, K., 1989, “Parameter Estimation for Flight Vehicles,”Journal of Guidance, Control, and Dynamics, Vol. 12. No. 5, pp. 609–622.

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