Evaluating H∞ controllers on the NRC Bell 205 fly-by-wire helicopter-Reference-Cited by-同舟云学术

Evaluating H∞ controllers on the NRC Bell 205 fly-by-wire helicopter

Published:2001-01 Issue:1 Volume:9 Page:1-10
ISSN:0967-0661
Container-title:Control Engineering Practice
language:en
Short-container-title:Control Engineering Practice

Author:

Smerlas A.J.,Walker D.J.,Postlethwaite I.,Strange M.E.,Howitt J.,Gubbels A.W.

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference18 articles.

1. Anon (1994). Aeronautical Design Standard ADS-33D - Handling Qualities Requirements for Military Helicopters. US Army, St. Louis, MO.

2. Baillie, S. W., Morgan, J. M., & Goheen, K. (1994). Practical experiences in control systems design using the NRC Bell 205 airborne simulator. Flight mechanics panel symposium (pp. 27.1–27.12).

3. Cooper, G. E., & Harper, R. P. (1969). The use of pilot rating in the evaluation of aircraft handling qualities. Technical Note TN D–5153, National Aeronautics and Space Administration, Washington, DC.

4. Heffley, R. K., Jewell, W. F., Lehman, J. F., & Van Winkle, R. A. (1979). A compilation and analysis of helicopter handling qualities data. NASA Contractor Report 3144, Systems Technology Inc., Mountain View, CA, US.

5. Hoyle, D., Hyde, R., & Limebeer, D. (1991). An H∞ approach to two degrees-of-freedom design. Proceedings of the 30th IEEE conference on decision and control, Brighton, UK (pp. 1581–1585).

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