Research of De-Couple Control System for near Space Vehicle with High Maneuver and Couple

Abstract:

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A de-couple control method with information feedback from other control channel and a method with double control loops were present for the hypersonic vehicle with non-linear, couple and lateral maneuver. The whole controller was divided into two parts: the computation of actuator which deal with control couple and design of control law which solve the problem of movement and aerodynamic couple. The time-varying controller parameter method and robust control law were present to solve the problem of quick time-varying model parameter and non-linear. Finally these two methods were analyzed contrastively; the simulation result show that these two methods present above can achieve the quick dynamic and high precise track of command. But the latter was better.

Info:

Periodical:

Edited by:

Zhixiang Hou

Pages:

979-984

DOI:

10.4028/www.scientific.net/AMM.128-129.979

Citation:

S. B. Ni et al., "Research of De-Couple Control System for near Space Vehicle with High Maneuver and Couple", Applied Mechanics and Materials, Vols. 128-129, pp. 979-984, 2012

Online since:

October 2011

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Price:

$35.00

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