Model Reference Control for Reducing Pilot-Induced Oscillation Tendencies Due to Actuator Rate Limits
AIAA SciTech Forum ; 2023 ; National Harbor, Md.; Online
2023
Aufsatz (Konferenz)
Englisch
Analysis of Pitch Pilot-Induced Oscillation Tendencies Due to Actuator Rate Limiting
British Library Conference Proceedings | 1999
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