The invention belongs to the technical field of remote sensing monitoring, and particularly relates to a gliding unmanned aerial vehicle launching system thrust measurement method. Pulleys are installed at the bottom of a base, the base achieves free linear motion on a rail through the pulleys, the base is connected with an electronic dynamometer through a connecting rod, and the output end of theelectronic dynamometer is connected with a computer through a data line. A launching system is fixed on the base in a bundling manner, so that the launching system and the base are firm and do not loosen; the method comprises the following steps: step 1, fixing the launching system on a measuring platform, and inserting an ignition device; step 2, sending an ignition signal to an ignition deviceby using control software, and sending a recording starting instruction to recording software at the same time; and 3, recording the thrust condition of the launching system after ignition by recording software, and drawing a graph by taking time as abscissa thrust as ordinate. The method has the characteristics of simple structure, convenient measurement and clear result recording.
本发明属于遥感监测技术领域,具体涉及一种测量滑翔无人机发射系统推力的方法。本发明中底座底部安装有滑轮,底座通过滑轮实现在轨道上的自由直线运动,底座通过连接杆与电子测力计相连,电子测力计的输出端通过数据线与计算机连接;发射系统采用捆扎方式固定在底座上,保证发射系统与底座之间牢固不松动;本发明方法包括如下步骤:步骤1,将发射系统固定在测量平台上,插上点火装置;步骤2,用控制软件向点火装置发送点火信号,同时向记录软件发送开始记录指令;步骤3,记录软件记录发射系统点火后的推力情况,并以时间作为横坐标推力为纵坐标作图。本发明具有结构简单,测量便捷,结果记录清晰的特点。
Gliding unmanned aerial vehicle launching system thrust measurement system and method
一种滑翔无人机发射系统推力测量系统及方法
16.10.2020
Patent
Elektronische Ressource
Chinesisch
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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