Carrier rocket information integration electrical system

The invention relates to a carrier rocket information integration electrical system consisting of an on-rocket centralized control device, a ground centralized control device, an on-rocket measurement and monitoring device and a ground measurement and monitoring device The on-rocket centralized control device automatically performs the centralized control of a carrier rocket in the carrier rocket flight process; the ground centralized control device controls the on-rocket work state during the ground testing; the on-rocket measurement and monitoring device monitors the running parameters of the systems of the rocket; the ground measurement and monitoring device is used to monitor the running parameters that characterize the working condition of the carrier rocket during the ground test; and the rocket and ground data communication of the whole electrical system is carried out via a 1553B bus, and the ground carries out the data communication via Ethernet. The carrier rocket electrical system is characterized