Robust full-envelope missile autopilot design

Jyh-Chin Juang, Ching Fang Lin, James R. Cloutier, Johnny H. Evers

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This paper delineates the design of a robust full-envelope autopilot of the HAVE DASH II missile system. Existing control design methods are examined and integrated to meet the stringent performance requirements of the missile autopilot design.

Original languageEnglish
Title of host publicationProceedings of the 1st IEEE Conference on Control Applications, CCA 1992
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages231-236
Number of pages6
ISBN (Electronic)0780300475, 9780780300477
DOIs
Publication statusPublished - 1992 Jan 1
Event1st IEEE Conference on Control Applications, CCA 1992 - Dayton, United States
Duration: 1992 Sep 121992 Sep 16

Publication series

NameProceedings of the 1st IEEE Conference on Control Applications, CCA 1992

Conference

Conference1st IEEE Conference on Control Applications, CCA 1992
CountryUnited States
CityDayton
Period92-09-1292-09-16

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering
  • Control and Optimization
  • Computer Science (miscellaneous)
  • Control and Systems Engineering
  • Aerospace Engineering
  • Industrial and Manufacturing Engineering

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  • Cite this

    Juang, J-C., Lin, C. F., Cloutier, J. R., & Evers, J. H. (1992). Robust full-envelope missile autopilot design. In Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992 (pp. 231-236). [269871] (Proceedings of the 1st IEEE Conference on Control Applications, CCA 1992). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCA.1992.269871