Journal of Astronautic Metrology and Measurement ›› 2023, Vol. 43 ›› Issue (6): 76-82.doi: 10.12060/j.issn.1000-7202.2023.06.14

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Research of Low Cost and High Integration for Launch Control System

WANG Xu1,RONG Gang1,CHANG Xi2,JIANG Yue1,MAI Ji2   

  1. 1.China Academy of Launch Vehicle Technology,Beijing 100076,China;
    2.Beijing Aerospace Institute for Metrology and Measurement Technology,Beijing 100076,China
  • Online:2023-12-25 Published:2023-12-25

Abstract: The design of the measuring,launching and control system of the vehicle is directly related to the efficiency and reliability of ground data transmission.A general low cost,high integration,integration system is proposed,which can realize real-time and post-hoc analysis and interpretation of test data while ensuring efficient transmission of time sequence instructions and telemetry data such as test power supply and distribution over long distances.Receiving the data on the aircraft,the fault detection,health status assessment,life and data management of the aircraft are completed by the ground measurement and control software.The system functions and software implementation methods are integrated to simplify the system architecture.The system development and maintenance costs are reduced,and the integration,reliability and maintenance of the system are improved.

Key words: Low cost, High integration, Integrated, Launch control system

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