Experimental Evaluation of High Bandwidth Helicopter Flight Control System Designs Exploiting Rotor State Feedback
Meeting, Innovation in rotorcraft technology ; 1997 ; London
Innovation in rotorcraft technology ; 17.1-17.13
01.01.1997
17.1-17.13
Aufsatz (Konferenz)
Englisch
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British Library Conference Proceedings | 1997
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