A guidance law design using the combination of ISMC and SDRE schemes

Yew-Wen Liang, Jun Yu Chen, Li Gang Lin

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

2 Scopus citations

Abstract

This paper studies the design of a robust guidance law for missiles in the presence of uncertainties, which may include inaccurate prediction of target maneuver. Under the design, the closed-loop guidance system is shown to be robust to the uncertainties. Additionally, the scheme presented possesses the flexibility of allowing the engineer to select a desired guidance law for the nominal system (i.e., system without uncertainty) so that the state response of the overall uncertain guidance system is close to that of the selected nominal closed-loop guidance system. The simulation results demonstrate the benefits of the presented scheme.

Original languageEnglish
Title of host publicationICSSE 2013 - IEEE International Conference on System Science and Engineering, Proceedings
Pages63-67
Number of pages5
DOIs
StatePublished - 18 Nov 2013
EventIEEE International Conference on System Science and Engineering, ICSSE 2013 - Budapest, Hungary
Duration: 4 Jul 20136 Jul 2013

Publication series

NameICSSE 2013 - IEEE International Conference on System Science and Engineering, Proceedings

Conference

ConferenceIEEE International Conference on System Science and Engineering, ICSSE 2013
CountryHungary
CityBudapest
Period4/07/136/07/13

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