The invention relates to a universal hypersonic flight test system, which comprises an effective load system, a ground system, a test carrying platform, a ground comprehensive control machine, a launch vehicle, a test launch control vehicle, a remote measurement vehicle and an external measurement vehicle, and is characterized in that the ground comprehensive control machine is a central node of the whole test system and is used for task planning, parameter instruction issuing and data recovery analysis; a test launch control front end and a carrier are arranged on the launch vehicle, the test launch control front end is used for executing instruction signals transmitted by the test launch control vehicle, the carrier comprises a carrying platform and a test load, the test load is installed in a fairing of the test platform, and the test platform provides a flight environment, power supply and communication conditions for the test load. The system provided by the invention adopts a universal and automatic design, the system works efficiently, and various hypersonic flight tests can be conveniently carried out.
本发明涉及一种通用化高超声速飞行试验系统,包括有效载荷系统、地面系统和试验运载平台,包括地面综控机、发射车、测发控车、遥测车和外测车,地面综控机是整个试验系统的中心节点,用于任务规划、参数指令下发和数据回收分析;发射车上设置测发控前端和运载器,测发控前端用于执行测发控车传递过来的指令信号,运载器包括运载平台和试验载荷,试验载荷安装于试验平台的整流罩内,试验平台为试验载荷提供飞行环境、供电和通信条件。本发明所提供的系统采用通用化和自动化设计,系统工作高效,方便开展各型高超声速飞行试验。
Universal hypersonic flight test system
一种通用化高超声速飞行试验系统
2023-07-11
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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