The invention provides a program control method and system for an autonomous sailboard after satellite and rocket separation. The program control method comprises the steps that S1, a satellite service computer periodically judges the satellite and rocket separation state; the satellite service computer carries satellite service software; s2, the satellite service computer issues an instruction based on the signal parameters, and panel expansion program control is completed; the signals comprise a posture in-place signal and an expansion in-place signal. The program control method suitable for the autonomous sailboard unfolding after the satellite and the rocket are separated is provided for the first time, the timeliness, safety and reliability of sailboard unfolding after the satellite and the rocket are separated can be improved, the pressure of ground measurement and control in the satellite launching and orbit injection section is relieved, a foundation is laid for smooth launching and orbit injection of the satellite, and the program control method has good engineering application value.

    本发明提供了一种用于卫星星箭分离后自主展帆板的程控方法及系统,包括步骤S1:星务计算机周期判断星箭分离状态;所述星务计算机搭载星务软件;步骤S2:星务计算机基于信号参数下达指令,完成帆板展开程控;所述信号包括姿态到位信号和展开到位信号。本发明首次提出一种适用于卫星星箭分离后自主展帆板的程控方法,能够提高星箭分离后帆板展开的及时性、安全性和可靠性,减轻卫星发射入轨段地面测控的压力,为卫星顺利发射入轨奠定基础,具有良好的工程应用价值。


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    Title :

    Program control method and system for autonomous sailboard after separation of satellite and rocket


    Additional title:

    用于卫星星箭分离后自主展帆板的程控方法及系统


    Contributors:
    HU BO (author) / LI RUIQIN (author) / ZHANG JUAN (author) / LI YINGJIE (author) / LI DONGWEI (author) / WANG ZIJUN (author) / ZHU WEI (author)

    Publication date :

    2024-03-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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