Linear parameter varying approach to gain scheduled missile autopilot design

Jeff S. Shamma*, James R. Cloutier

*Corresponding author for this work

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

39 Scopus citations

Abstract

This paper presents a gain-scheduled design for a missile longitudinal autopilot. The gain-scheduled design is novel in that it does not involve linearizations about trim conditions of the missile dynamics. Rather, the missile dynamics are brought to a quasi-linear parameter varying (LPV) form via a state transformation. An LPV system is defined as a linear system whose dynamics depend on an exogenous variable whose values are unknown a priori but can be measured upon system operation. In this case, the variable is the angle-of-attack. This is actually an endogenous variable, hence the expression ``quasi-LPV''. Once in a quasi-LPV form, a robust controller using μ-synthesis is designed to achieve normal acceleration control via fin deflections. The final design is an inner/outer loop structure, with angle-of-attack control being the inner-loop, and normal-acceleration control being the outer loop.

Original languageEnglish (US)
Title of host publicationProceedings of the American Control Conference
PublisherPubl by American Automatic Control Council
Pages1317-1321
Number of pages5
Volume2
ISBN (Print)0780302109
StatePublished - 1992
Externally publishedYes
EventProceedings of the 1992 American Control Conference - Chicago, IL, USA
Duration: Jun 24 1992Jun 26 1992

Other

OtherProceedings of the 1992 American Control Conference
CityChicago, IL, USA
Period06/24/9206/26/92

ASJC Scopus subject areas

  • Control and Systems Engineering

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