Aircraft rocket control system for aircraft multi-mode switching in full life cycle

According to the aircraft on-rocket control system for aircraft multi-mode switching in the whole life cycle, the system adopts a three-stage cabin body structure, and the three-stage cabin body comprises a first-stage boosting power cabin body, a second-stage maneuvering control cabin body and a third-stage load gliding target control cabin body; the first-stage boosting power cabin is used for performing high-thrust flight control of an active section and recovery control of the first-stage boosting power cabin after the aircraft takes off; and the second-stage maneuvering control cabin and the third-stage load gliding target control cabin are both used for controlling the flight of a level flight layer of the aircraft and controlling the load to enter a preset orbit. The automatic and real-time supervision of the variation trend of the degradation of the multi-mode switching system of the aircraft can be realized. 本公开的用于全寿命周期的飞行器多模态切换的飞行器箭上控制系统，所述系统采用三级舱体结构，所述三级舱体包括一级助推动力舱体、二级机动控制舱体和三级载荷滑翔目标控制舱体；所述一级助推动力舱体