A New Optimal Control Algorithm for Quad-rotor Helicopter with State Constraints via Sliding-mode Control

A New Optimal Control Algorithm for Quad-rotor Helicopter with State Constraints via Sliding-mode Control

This paper proposes a strategy of a new optimal sliding-mode control for flight control system with state constraints so that the system guarantees the optimal performance index. Besides, the strategy ensures strong robustness to the internal parametric uncertainty and the external disturbances. In...

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Bibliographic Details
Main Authors: Zhao Jing, Yang Pu, Zhang Zecheng, Liu Jianwei
Format: Article
Language:English
Published: EDP Sciences 2015-01-01
Series:MATEC Web of Conferences
Subjects:
flight control system
state constraint
sliding-mode control
optimal control
quad-rotor helicopter
Online Access:http://dx.doi.org/10.1051/matecconf/20152203008

Internet

http://dx.doi.org/10.1051/matecconf/20152203008

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