The invention discloses a ground test platform and method for aircraft dynamics and control integrated research, and relates to the fields of machinery, aircraft dynamics and control technologies, information technologies, test technologies and the like. The ground test platform for aircraft dynamics and control integrated research comprises a supporting base, a moving part, a sensor part and a control part, wherein the sensor part is mainly a force measuring part; the supporting base is used for installing a force measuring component, and the force measuring component is used for installing a moving component; the moving part is used for mounting a to-be-tested element; and the control part receives a signal transmitted by the sensor part and generates a control instruction to control the to-be-tested element. Based on the test platform, the test platform can be used for assembling required moving parts, so that the test of different to-be-tested elements is realized.
本发明公开了一种用于飞行器动力学与控制一体化研究的地面试验平台、方法,涉及机械、飞行器动力学与控制技术、信息技术、测试技术等领域。所述用于飞行器动力学与控制一体化研究的地面试验平台包括支撑底座、运动部件、传感器部件、控制部件,所述传感器部件主要是测力部件;所述支撑底座上用于安装测力部件,所述测力部件上用于安装运动部件;所述运动部件用于安装待测元件;所述控制部件接受传感器部件传递的信号,生成控制指令控制待测元件。基于该试验平台可以用于装配所需要的运动部件,进而实现不同待测元件的试验。
Ground test platform and method for aircraft dynamics and control integrated research
用于飞行器动力学与控制一体化研究的地面试验平台、方法
29.12.2023
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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