System identification requirements for high-bandwidth rotorcraft flight control system design
- 1 September 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 13 (5) , 835-841
- https://doi.org/10.2514/3.25409
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Influence of high-order dynamics on helicopter flight-control systembandwidthJournal of Guidance, Control, and Dynamics, 1986
- Inclusion of Rotor Dynamics in Controller Design for HelicoptersJournal of Aircraft, 1973