A launch vehicle digital power supply and distribution control system and its test method
A technology for a launch vehicle and a control system, applied in the aerospace field, can solve the problems of large size of electromagnetic relays, large influence of switching transient effect test results, and occupation of space on the arrow, so as to save space and load on the arrow, and accurately respond to Emergency situations, the effect of reducing electromagnetic interference
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Embodiment 1
[0035] The application provides a digital power supply and distribution control system for a launch vehicle, including a power distribution control system for intelligent equipment and a power distribution control system for pyrotechnics. The length of the launch vehicle is relatively long, so the two ends of the rocket are respectively equipped with an intelligent equipment power distribution control system and an explosive power distribution control system. Such as figure 1 , 2 As shown, the intelligent device power distribution control system and the pyrotechnic product power distribution control system are respectively equipped with an instrument battery 11 and a pyrotechnic battery 21, so as to reduce the power consumption of the intelligent device power distribution control system and the pyrotechnic product power distribution control system powered by the same battery. Voltage loss due to long cables.
[0036] Both the intelligent equipment power distribution control ...
Embodiment 2
[0047] The present application also provides a test method for the digitalized power supply and distribution control system of the launch vehicle matched with the digitalized power supply and distribution control system of the launch vehicle in Embodiment 1.
[0048] The ground measurement and control system sends commands to close or disconnect each switch to the intelligent equipment power distribution control system and the pyrotechnic power distribution control system through Ethernet;
[0049] Each switch combination in the digital power supply and distribution control system of the launch vehicle executes the command after receiving the command;
[0050] Such as image 3 , 4 As shown, the data collection points 13, 14, 15, 23, and 24 are connected to the ground measurement and control communication, and the collection points 13, 14, 15, 23, and 24 are used to transmit the collected data to the ground measurement and control via Ethernet. Launch control, the data is dis...
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