Synthesis of Helicopter Stabilization Systems Using Modal Control Theory
- 1 January 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (1) , 3-8
- https://doi.org/10.2514/3.58931
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Design of helicopter stabilization systems using optimal control theory.Journal of Aircraft, 1969
- A theory of modal controlInformation and Control, 1968