The invention discloses a liquid recoverable carrier
rocket control system and control method, and belongs to the technical field of
rocket recovery control. Comprising a flight control combination, a
recovery control combination, an
inertia measurement combination, a battery, a
safety control combination, an engine controller, an optical target camera, a
laser range finder, a comprehensive collecting and editing device, a
relay measurement and control terminal and a space-based telemetering
phased array antenna. The flight control combination and the
recovery control combination are arranged in the second
rocket sublevel and the first rocket sublevel respectively, partial hot
backup is achieved through the two control combinations, and the reliability of the
system is improved. In the first-stage flight section with the worst and most dangerous mechanical environment, the recovery control combination can serve as hot
backup execution work of the flight control combination, and normal recovery of the first sub-stage cannot be affected even if flight failure is caused by abnormity of the second-stage rocket. Effective control over launch and recovery of the carrier rocket can be met, and a necessary
control system is provided for recovery of the carrier rocket.