Understanding missile autopilot design using the H loop shaping design procedure

Thomas J. Urban, Pete Iwaskiw, Pablo A. Iglesias

Research output: Contribution to conferencePaper

Abstract

This paper presents different controller topologies for a missile autopilot. The controllers are based on a loop shaping design procedure due to McFarlane and Glover. The nature of the controllers obtained is discussed and a novel procedure for the selection of weights is given.

Original languageEnglish (US)
Pages236-242
Number of pages7
StatePublished - Dec 1 1999
EventProceedings of the 1999 IEEE International Conference on Control Applications (CCA) and IEEE International Symposium on Computer Aided Control System Design (CACSD) - Kohala Coast, HI, USA
Duration: Aug 22 1999Aug 27 1999

Other

OtherProceedings of the 1999 IEEE International Conference on Control Applications (CCA) and IEEE International Symposium on Computer Aided Control System Design (CACSD)
CityKohala Coast, HI, USA
Period8/22/998/27/99

ASJC Scopus subject areas

  • Control and Systems Engineering

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    Urban, T. J., Iwaskiw, P., & Iglesias, P. A. (1999). Understanding missile autopilot design using the H loop shaping design procedure. 236-242. Paper presented at Proceedings of the 1999 IEEE International Conference on Control Applications (CCA) and IEEE International Symposium on Computer Aided Control System Design (CACSD), Kohala Coast, HI, USA, .