Overload Control of Supersonic Missile System

Yu Qiang Jin; Qiang Ma

doi:10.4028/www.scientific.net/AMR.295-297.1761

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 295-297Overload Control of Supersonic Missile System

Overload Control of Supersonic Missile System

Abstract:

PI control is also an old and classic method which is effective and mostly used in linear systems. In this paper, two assumptions are proposed to simplify the design of overload control system of supersonic missiles. No aero-coefficient is necessary to be known because of the adopting of PI control method.

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Periodical:

Advanced Materials Research (Volumes 295-297)

Pages:

1761-1763

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.295-297.1761

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Online since:

July 2011

Authors:

Yu Qiang Jin, Qiang Ma

Keywords:

Backstepping, Nonlinear, Overload Control, Supersonic Missile, Uncertainty

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