Design of multi-mode flight control system for unmanned helicopter

Author

Xu Hongzhe ; Huang Jim ; Zhou Yaoming

Author_Institution

Dept. of Aeronaut. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China

fYear

2011

fDate

22-24 July 2011

Firstpage

3660

Lastpage

3663

Abstract

Based on the special requirements of flight control and navigation system of unmanned helicopter, this paper present the main framework of flight control system in a certain type of unmanned helicopter, proposed three flight control modes based on different design stages, gave the autonomous control algorithm and the smoothing method while switching between remote control mode and stability augmentation mode, ultimately proved the feasibility of flight control and navigation program through the semi-physical simulation test and flight test.

Keywords

aerospace robotics; aircraft control; control system synthesis; helicopters; mobile robots; path planning; remotely operated vehicles; stability; telerobotics; autonomous control algorithm; flight test; multimode flight control system design; navigation system; remote control mode; semiphysical simulation test; smoothing method; stability augmentation mode; unmanned helicopter; Aerospace control; Computational modeling; FCC; Helicopters; Servomotors; Switches; Autonomous Control; FCC; Flight Control; Semi-physical Simulation; Stability Augmentation;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2011 30th Chinese

Conference_Location

Yantai

ISSN

1934-1768

Print_ISBN

978-1-4577-0677-6

Electronic_ISBN

1934-1768

Type

conf

Filename

6001612