Design of Variable Structure Control Law of a Guidance Missile

Qi Wang*, Xiuyun Meng

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

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).

Original languageEnglish
Title of host publicationProceedings of the International Symposium on Test and Measurement
Pages1223-1226
Number of pages4
Publication statusPublished - 2003

Publication series

NameProceedings of the International Symposium on Test and Measurement
Volume2

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