Understanding missile autopilot design using the H∞ loop shaping design procedure

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

Understanding missile autopilot design using the H_∞ loop shaping design procedure

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

Whiting School of Engineering

Research output: Contribution to conference › Paper › peer-review

5 Scopus citations

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 language	English (US)
Pages	236-242
Number of pages	7
State	Published - Dec 1 1999
Event	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 Duration: Aug 22 1999 → Aug 27 1999

Other

Other	Proceedings of the 1999 IEEE International Conference on Control Applications (CCA) and IEEE International Symposium on Computer Aided Control System Design (CACSD)
City	Kohala Coast, HI, USA
Period	8/22/99 → 8/27/99

ASJC Scopus subject areas

Control and Systems Engineering

Cite this

Understanding missile autopilot design using the H_∞ loop shaping design procedure. / Urban, Thomas J.; Iwaskiw, Pete; Iglesias, Pablo A.
1999. 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.

Research output: Contribution to conference › Paper › peer-review

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AU - Iwaskiw, Pete

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Y2 - 22 August 1999 through 27 August 1999

ER -

Understanding missile autopilot design using the H_∞ loop shaping design procedure

Abstract

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ASJC Scopus subject areas

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