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

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/autopil...

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Bibliographic Details

Published in:	2011 3rd International Conference on Computer Research and Development Vol. 4; pp. 431 - 435
Main Authors:	Jinyong Yu, Qingjiu Xu, Yue Zhi
Format:	Conference Proceeding
Language:	English
Published:	IEEE 01.03.2011
Subjects:	Aerodynamics Backstepping Integrated guidance/autopilot design Manifolds Simulation Sliding mode control Switches Terminal sliding-mode control
ISBN:	1612848397, 9781612848396
Online Access:	Get full text
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