Autonomous flight control system designed for small-scale helicopter based on approximate dynamic inversion

This paper describes the development of an autonomous flight control system for small-scale unmanned helicopter based on approximate dynamic inversion (ADI) method. The flight controller consists of inner-loop attitude control, mid-loop velocity control and outer-loop position control. Previous rese...

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Veröffentlicht in:	2011 3rd International Conference on Advanced Computer Control S. 185 - 191
Hauptverfasser:	Zhiyang Zhang, Fei Hu, Jian Li
Format:	Tagungsbericht
Sprache:	Englisch
Veröffentlicht:	IEEE 01.01.2011
Schlagworte:	Approximate Dynamic Inversion Flight Control Gold Helicopters Mathematical model MATLAB Proportional-Integral UAV Helicopter
ISBN:	1424488095, 9781424488094
Online-Zugang:	Volltext
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