The hardware construction and algorithm design of control system in small unmanned gyroplane

Author

Bohu Zhang ; Hui Xu

Author_Institution

Commun. Eng. Dept., Armed Police Force Eng. Coll., Xi´an, China

fYear

2011

fDate

19-22 Aug. 2011

Firstpage

568

Lastpage

571

Abstract

The flight control system is the core of small unmanned gyroplane, in this paper, micro controller AT91M55800A chosen from ARM7 series is used to construct the control platform. In order to improve the stability and robustness of small unmanned gyroplane, this paper puts forward a kind of PID controller which based on improved Differential Evolution Algorithm so that the gyroplane can finally achieve the optimal control.

Keywords

aerospace robotics; aircraft control; control system synthesis; evolutionary computation; microcontrollers; mobile robots; optimal control; remotely operated vehicles; robust control; three-term control; ARM7 series; AT91M55800A microcontroller; PID controller; control platform; control system design; differential evolution algorithm; flight control system; hardware construction; optimal control; robustness; small unmanned gyroplane; stability; Aerospace control; Algorithm design and analysis; Control systems; Global Positioning System; Hardware; Random access memory; Robustness; PID controller; flight control; improved Differential Evolution Algorithm; small unmanned gyroplane;

fLanguage

English

Publisher

ieee

Conference_Titel

Mechatronic Science, Electric Engineering and Computer (MEC), 2011 International Conference on

Conference_Location

Jilin

Print_ISBN

978-1-61284-719-1

Type

conf

DOI

10.1109/MEC.2011.6025528

Filename

6025528