Work

Integral Sliding Mode Control of Airship Pitch Channel simplified model

Year: 2016

Type: conference-paper

Abstract: A kind of integral type sliding mode control law was designed for a kind of simplified pitch channel model of hypersonic aircraft which is widely discussed recently.The advantage of sliding mode control is that it has strong robustness.And the integral sliding mode control method can reduce steady state error.And with the help of constructing two Lyapunov functions, all signals of close system are proved to be stable.At last, detailed simulation was done to testify the rightness of the proposed method.

Source: Advances in engineering research/Advances in Engineering Research

DOI: 10.2991/icmmct-16.2016.9

Authors: Aijun Zhou, Junbo Chu, Haibo Wang, Tianwei Li, Guoqiang Liang

Institutions: Dalian Naval Academy, Naval Aeronautical and Astronautical University

Language: English

Topic: Adaptive Control of Nonlinear Systems

Subfield: Control and Systems Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: hybrid

OpenAlex ID: W2323611908

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Cites: 14

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Related to: 10