A TSM control scheme of integrated guidance/autopilot design for UAV

Author

Yu, Jinyong ; Xu, Qingjiu ; Zhi, Yue

Author_Institution

Dept. of Control Eng., Naval Aeronaut. & Astronaut. Univ., Yantai, China

Volume

4

fYear

2011

fDate

11-13 March 2011

Firstpage

431

Lastpage

435

Abstract

A scheme for integrated guidance/autopilot design for some UAV based on terminal sliding-mode(TSM) control is proposed. Firstly, the terminal sliding mode control is introduced, then a guidance/control law is designed based on TSM control and the backstepping idea when an integrated guidance/autopilot model on the yaw plane of some UVA is formulated. Secondly, for the unavailable information of the maneuvering target, an estimating method is given and an auxiliary control based on a sliding mode estimator is used to offset the estimation error. Finally, a simulation of some UAV against high maneuvering targets on the yaw plane was made to verify the effectiveness and rightness of the scheme, and the simulation results have shown that good offensive performance can be got.

Keywords

aircraft landing guidance; estimation theory; mobile robots; remotely operated vehicles; variable structure systems; TSM control; UAV; auxiliary control; estimating method; estimation error; integrated guidance-autopilot design; sliding mode estimator; terminal sliding mode control; yaw plane; Aerodynamics; Backstepping; Manifolds; Simulation; Sliding mode control; Switches; Backstepping; Integrated guidance/autopilot design; Terminal sliding-mode control;

fLanguage

English

Publisher

ieee

Conference_Titel

Computer Research and Development (ICCRD), 2011 3rd International Conference on

Conference_Location

Shanghai

Print_ISBN

978-1-61284-839-6

Type

conf

DOI

10.1109/ICCRD.2011.5763939

Filename

5763939