This paper describes the implementation of an automatic position-hold system in the NASA/Army CH47B variable-stability research helicopter. The test helicopter is briefly described, and a detailed documentation is given of the position-measurement system. The control system design model and the design procedure are described, and flight-test data describing overall system performance in strong winds are presented.
Development and flight test of a precision autohover capability for tactical rotorcraft
1988-06-01
Conference paper
No indication
English
Rotorcraft Tactical Simulation Modelling Fidelity Issues
British Library Conference Proceedings | 1994
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