Design of an axially telescoping wing control system based on servo motor

Author

Chen, Xi ; Zhang, Wei ; Cao, Dongxing

Author_Institution

Coll. of Mech. Eng., Beijing Univ. of Technol. (BJUT), Beijing, China

fYear

2011

fDate

15-17 July 2011

Firstpage

1169

Lastpage

1172

Abstract

In this paper, a control system of axially telescoping wing experimental device is investigated. The control system is composed of STC89C52 SCM, an AC servo motor and two margin micro-switches. Based on the experimental device, a new design of telescoping wing is given. Telescoping wing is a kind of morphing wing, and is represented by an axially moving cantilever beam/plate. Telescoping wing is able to change its wing area and aspect ratio in order to adapt to the variable environments. The extending and retracting of telescoping wings could accomplish different actions and meet diverse needs in variable flight environments. Thus, the research of retractable wing is of great significance for both theory study and practical application.

Keywords

aerospace components; aerospace control; microcontrollers; servomotors; AC servomotor; STC89C52 SCM microcontroller; axially moving cantilever beam; axially moving cantilever plate; axially telescoping wing control system; margin microswitch; morphing wing; telescoping wing extension; telescoping wing retraction; variable flight environment; Circuit synthesis; Induction motors; Position control; Servomotors; Software design; AC servo motor; SCM; axially moving cantilever beam/plate; morphing wing;

fLanguage

English

Publisher

ieee

Conference_Titel

Mechanic Automation and Control Engineering (MACE), 2011 Second International Conference on

Conference_Location

Hohhot

Print_ISBN

978-1-4244-9436-1

Type

conf

DOI

10.1109/MACE.2011.5987145

Filename

5987145