05.1 - Flight Dynamics and Control (Control & Modelling)
TERMINAL IMPACT ANGLE AND ANGLE-OF-ATTACK CONTROL GUIDANCE FOR SURFACE-TO-AIR MISSILE USING TVC
S.-M. Hong¹, M.-G. Seo¹, M.-J. Tahk¹; ¹KAIST, South Korea
This paper deals with impact time and angle control guidance for two-staged surface-to-air missile. Terminal impact angle constraint should be satisfied within limited burntime. To make a stage separation stable, angle-of-attack should be zero. To satisfy all constraints as mentioned above, existing impact time and angle control guidance law is modified based on optimal control theory.