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...

Full description

Bibliographic Details

Published in:	2011 3rd International Conference on Advanced Computer Control pp. 185 - 191
Main Authors:	Zhiyang Zhang, Fei Hu, Jian Li
Format:	Conference Proceeding
Language:	English
Published:	IEEE 01.01.2011
Subjects:	Approximate Dynamic Inversion Flight Control Gold Helicopters Mathematical model MATLAB Proportional-Integral UAV Helicopter
ISBN:	1424488095, 9781424488094
Online Access:	Get full text
Tags:	Add Tag No Tags, Be the first to tag this record!