Experimental study of a helicopter rotor model in hover
نویسندگان
چکیده
منابع مشابه
Helicopter Rotor Airloads Prediction Using CFD and Flight Test Measurement in Hover Flight
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A state-space model for a small radio-controlled helicopter in hover is developed. Linear estimation is used to identify parameters of the model. The parameter variances are used to develop an uncertainty description of the system. An LQG controller with setpoint tracking is designed and implemented on this system.
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ژورنال
عنوان ژورنال: MATEC Web of Conferences
سال: 2018
ISSN: 2261-236X
DOI: 10.1051/matecconf/201823401002