Design of Variable Structure Control Law of a Guidance Missile

Qi Wang; Xiuyun Meng

Design of Variable Structure Control Law of a Guidance Missile

Qi Wang^*
, Xiuyun Meng

^*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: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

In this paper, a novel guidance law based on Line of Sight from the launching station to the target by using variable structure control (VSC) is proposed. The basic feature of VSC is the sliding motion. Sliding Mode Controller (SMC) are robust, simple guidance and control algorithms which can be applied to anti-tank missiles. Here we design the guidance control law for high speed kinetic energy anti-tank missiles (HKEM).

源语言	英语
主期刊名	Proceedings of the International Symposium on Test and Measurement
页	1223-1226
页数	4
出版状态	已出版 - 2003

丛书

姓名	Proceedings of the International Symposium on Test and Measurement
卷	2

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@inproceedings{760d8a985abd40eb911691c017540744,

title = "Design of Variable Structure Control Law of a Guidance Missile",

abstract = "In this paper, a novel guidance law based on Line of Sight from the launching station to the target by using variable structure control (VSC) is proposed. The basic feature of VSC is the sliding motion. Sliding Mode Controller (SMC) are robust, simple guidance and control algorithms which can be applied to anti-tank missiles. Here we design the guidance control law for high speed kinetic energy anti-tank missiles (HKEM).",

author = "Qi Wang and Xiuyun Meng",

year = "2003",

language = "English",

series = "Proceedings of the International Symposium on Test and Measurement",

pages = "1223--1226",

booktitle = "Proceedings of the International Symposium on Test and Measurement",

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TY - GEN

T1 - Design of Variable Structure Control Law of a Guidance Missile

AU - Wang, Qi

AU - Meng, Xiuyun

PY - 2003

Y1 - 2003

N2 - In this paper, a novel guidance law based on Line of Sight from the launching station to the target by using variable structure control (VSC) is proposed. The basic feature of VSC is the sliding motion. Sliding Mode Controller (SMC) are robust, simple guidance and control algorithms which can be applied to anti-tank missiles. Here we design the guidance control law for high speed kinetic energy anti-tank missiles (HKEM).

AB - In this paper, a novel guidance law based on Line of Sight from the launching station to the target by using variable structure control (VSC) is proposed. The basic feature of VSC is the sliding motion. Sliding Mode Controller (SMC) are robust, simple guidance and control algorithms which can be applied to anti-tank missiles. Here we design the guidance control law for high speed kinetic energy anti-tank missiles (HKEM).

UR - https://www.scopus.com/pages/publications/0141426420

M3 - Conference contribution

AN - SCOPUS:0141426420

T3 - Proceedings of the International Symposium on Test and Measurement

SP - 1223

EP - 1226

BT - Proceedings of the International Symposium on Test and Measurement

ER -

Design of Variable Structure Control Law of a Guidance Missile

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丛书

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