Test bench for rotorcraft hover control
- 1 July 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 17 (4) , 729-736
- https://doi.org/10.2514/3.21261
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
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- Design of attitude and rate command systems for helicopters using eigenstructure assignmentJournal of Guidance, Control, and Dynamics, 1989
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- Right half plane poles and zeros and design tradeoffs in feedback systemsIEEE Transactions on Automatic Control, 1985