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Guidance law to guide the unpowered flight vehicle to attack ground target vertically is needed in modem warfare, and hybrid BTT/STT guidance command allocation is also needed to reduce the response time of the guidance system. A guidance law design method based on Lyapunov stability theory is proposed, and a guidance law with sight angle and sight angle velocity as feedback variables is designed...
An integrated guidance and control (IGC) method for bank to turn (BTT) flight vehicle with impact angle constraint is presented, using multiple sliding surface control theory. Based on missile-target engagement geometry model and BTT control mode, an IGC model is formulated. According to multiple sliding surfaces control theory, IGC laws are designed in pitch channel and roll-yaw channels respectively...
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