DocumentCode :
2705040
Title :
Design of hovering altitude holding control system for helicopter
Author :
Wang, Xiaoyan ; Wang, Xinmin ; Yao, Congchao
Author_Institution :
Dept. of Autom., Northwestern Polytech. Univ., Xi´´an, China
fYear :
2012
fDate :
6-8 June 2012
Firstpage :
180
Lastpage :
183
Abstract :
Effected by sea wave and other noises, altitude holding becomes difficult when helicopter is hovering or rescuing near the sea face. In this paper, according to the integrated height system of radio altimeter and vertical accelerometer, a Kalman filter is designed to get the accurate altitude signals of the helicopter hovering over the sea. Then, two altitude holding control structures are developed based on helicopter explicit model following control system (EMFCS), which has excellent operation characteristics. In order to simulate the real situation and to design the filter, sea wave model is established by using the rational spectrum modeling method. Simulation results show that the two control systems designed both can realize helicopter hovering altitude holding efficiently, and have good resistance to vertical wind disturbance or parametric perturbations.
Keywords :
Kalman filters; aircraft control; helicopters; ocean waves; position control; EMFCS; Kalman filter; helicopter explicit model following control system; helicopter hovering; hovering altitude holding control system; integrated height system; parametric perturbations; radio altimeter; rational spectrum modeling method; sea wave model; vertical accelerometer; vertical wind disturbance; Filtering theory; Helicopters; Mathematical model; Noise measurement; Sea measurements; White noise; altitude holding; filter; helicopter; hovering; wave model;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Information and Automation (ICIA), 2012 International Conference on
Conference_Location :
Shenyang
Print_ISBN :
978-1-4673-2238-6
Electronic_ISBN :
978-1-4673-2236-2
Type :
conf
DOI :
10.1109/ICInfA.2012.6246804
Filename :
6246804
Link To Document :
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