Research on Accessibility of Integral Sliding Mode Contorl of Missile System

Abstract:

Considering the no uncertain air-dynamic coefficients situation, a kind of sliding mode control law, which was composed of the angle velocity and overload error, was designed for the overload control system of missile. And the accessibility of sliding mode was analyzed. What worthy pointing out is that a transfer- function-type backstepping algorithm was adopted to solve the derivative item of actuator and a novel type of control was proposed.

• Periodical: Applied Mechanics and Materials (Volumes 66-68)
• Pages: 212-216
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.66-68.212
• Online since: July 2011
• Authors: Wen Guang Zhang, Jun Wei Lei, Ling Ling Wang
• Keywords: Angle Velocity, Overload Control, Sliding Mode, Stability

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