Development and flight testing of quantitative feedback theory pitch rate stability augmentation system
Authors:
- 1 September 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 19 (5) , 1109-1115
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Design of robust quantitative feedback theory controllers for pitch attitude hold systemsJournal of Guidance, Control, and Dynamics, 1994
- Benchmark problem solution by quantitative feedback theoryJournal of Guidance, Control, and Dynamics, 1992
- A quantitative design method for MIMO linear feedback systems having uncertain plantsInternational Journal of Control, 1986
- Quantitative synthesis of uncertain multiple input-output feedback systemInternational Journal of Control, 1979
- Synthesis of feedback systems with large plant ignorance for prescribed time-domain tolerances†International Journal of Control, 1972