Quantitative feedback theory applied to the design of a rotorcraft flight control system
- 1 July 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 16 (4) , 748-753
- https://doi.org/10.2514/3.21076
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Invited paper Survey of quantitative feedback theory (QFT)International Journal of Control, 1991
- Reduced-order modeling and controller design for a high-performance helicopterJournal of Guidance, Control, and Dynamics, 1990
- Design of attitude and rate command systems for helicopters using eigenstructure assignmentJournal of Guidance, Control, and Dynamics, 1989
- Quantitative feedback theoryIEE Proceedings D Control Theory and Applications, 1982
- Design of a 3×3 multivariable feedback system with large plant uncertainty†International Journal of Control, 1981
- Synthesis of feedback systems with large plant ignorance for prescribed time-domain tolerances†International Journal of Control, 1972