27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-5.6.2

SUB-OPTIMAL MISSILE GUIDANCE WITH PULSE-MOTOR CONTROL LOGIC USING THE SINGULAR PERTURBATIONS METHOD

E. Sigal, J. Z. Ben-Asher
Technion, Israel

Keywords: missile guidance, control, perturbations method

This study deals with the planar non linear guidance problem for an interception missile. The model includes a controlable two pulse rocket motor. The proposed solution method is based on formulation of the problem as a switched system. A sub optimal solution using the singular perturbation method is presented.

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