Model Reference Control for Reducing Pilot-Induced Oscillation Tendencies Due to Actuator Rate Limits
AIAA SCITECH 2023 Forum
01.01.2023
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Analysis of Pitch Pilot-Induced Oscillation Tendencies Due to Actuator Rate Limiting
British Library Conference Proceedings | 1999
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