Integrated test launch control method and device for liquid carrier rocket

Abstract

The invention discloses an integrated measurement, launch and control method and device for a liquid carrier rocket. The device comprises a first measurement and control combination and a second measurement and control combination which are connected with each other through a cable. The first measurement and control combination is in network connection with the rear-end control computer, is in cable connection with the liquid carrier rocket, and is used for receiving control of the rear-end control computer and performing related detection and control on an electrical system on the rocket in the measurement and launching process of the liquid carrier rocket; the second measurement and control combination is in network connection with the rear-end control computer, is in cable connection with a ground controlled object, and is used for receiving the control of the rear-end control computer and performing related detection and control on the ground controlled object in the measurement and launch process of the liquid carrier rocket; therefore, the ground controlled object and the rocket electrical system are matched with each other in the testing and launching process of the liquid carrier rocket.

Description

technical field [0001] The present application relates to the field of aerospace technology, in particular to an integrated measurement, launch and control method and equipment for liquid launch vehicles. Background technique [0002] With the continuous development of aerospace technology, my country's rocket launch business is becoming more and more mature. Since the launch of a rocket is a complex process, it needs the cooperation between the rocket and the ground to complete. During this period, because the related systems are independent of each other, there are a lot of information interaction links between the related systems, there are many equipments, and the command passwords are complicated. If there is a delay or error in the cooperation between the related systems, it will lead to a serious launch accident. [0003] Therefore, how to improve the integration of various related systems in the process of rocket testing and launch, and prevent rocket launch acciden...

AI Technical Summary

Problems solved by technology

[0004] The present invention provides an integrated measurement, launch and control method and equipment for liquid carrier rockets to solve or partially solve the problem of rocket failure caused by system coordination problems caused by the low degree of integration of various related systems during the rocket's measurement and launch process. The technical problems of launch accidents, and then improve the safety of the rocket during the test and launch process

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