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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Summary: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.
ISBN:1612848397
9781612848396
DOI:10.1109/ICCRD.2011.5763939