Study on Integrated Flight/Propulsion Control Method of Compound Adjustable Ducted Rocket

摘要

For the integrated control of the missile and the compound adjustable ducted rocket, the Integrated Flight/Propulsion Control (1FPC) system was constructed by hierarchical dispersion method based on the mathematical model of the system and the coupling characteristics analysis between the subsystems. According to the work principle of the integrated system, the integration and the coordination of the subsystems were achieved by the motion control commands and the coordination control commands respectively. The IFPC method was validated by simulation based on typical mission. The results show that the IFPC system can control the motion of the missile and coordinate the operating status of the subsystems effectively.