A composite sliding mode autopilot design

Qunli Xia; Jingju Zhu; Zaikang Qi

doi:10.1504/IJMIC.2010.032358

A composite sliding mode autopilot design

Qunli Xia^*
, Jingju Zhu
, Zaikang Qi

^*此作品的通讯作者

空天科学与技术学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

摘要

Sliding mode control has been applied to the design of many missile autopilots. In this paper, a control method with the primary feedback being proportional to the switching is developed for eliminating the disturbance effect due to model uncertainty. With this control method, a sliding mode autopilot is analysed. Then, a composite sliding mode control strategy is discussed to reduce the switching frequency. Numerical simulation results show a good performance of the composite control system.

源语言	英语
页（从-至）	37-42
页数	6
期刊	International Journal of Modelling, Identification and Control
卷	9
期	1-2
DOI	https://doi.org/10.1504/IJMIC.2010.032358
出版状态	已出版 - 4月 2010

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title = "A composite sliding mode autopilot design",

abstract = "Sliding mode control has been applied to the design of many missile autopilots. In this paper, a control method with the primary feedback being proportional to the switching is developed for eliminating the disturbance effect due to model uncertainty. With this control method, a sliding mode autopilot is analysed. Then, a composite sliding mode control strategy is discussed to reduce the switching frequency. Numerical simulation results show a good performance of the composite control system.",

keywords = "Composite sliding mode, Missile autopilot, Model uncertainty, Sliding mode control",

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AB - Sliding mode control has been applied to the design of many missile autopilots. In this paper, a control method with the primary feedback being proportional to the switching is developed for eliminating the disturbance effect due to model uncertainty. With this control method, a sliding mode autopilot is analysed. Then, a composite sliding mode control strategy is discussed to reduce the switching frequency. Numerical simulation results show a good performance of the composite control system.

KW - Composite sliding mode

KW - Missile autopilot

KW - Model uncertainty

KW - Sliding mode control

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A composite sliding mode autopilot design

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