The invention provides a test system for simulating low-gravity landing of the moon, which comprises a comprehensive control subsystem, an inclined platform subsystem, a speed-up subsystem, a protection subsystem, a measurement subsystem, a simulator and a simulated landing surface subsystem, and is characterized in that the comprehensive control subsystem, the inclined platform subsystem, the protection subsystem and the simulated landing surface subsystem are mounted on the ground; the measuring subsystem is installed on the top of the protection subsystem, the speed-up subsystem is installed in the middle of the protection subsystem, and a speed-up pull rod of the speed-up subsystem is connected with an electromagnet connecting piece of the simulator through an electromagnet, so that cooperation between the speed-up subsystem and the simulator is achieved. A landing leg assembly of the simulator acts on the inclined platform subsystem; the plane air cushion of the simulator acts on the inclined platform subsystem. According to the invention, simulator landing tests under different speed combinations and different terrains are realized.
本发明提供了一种用于模拟月球低重力着陆的试验系统,包括综控子系统、倾斜平台子系统、起速子系统、防护子系统、测量子系统、模拟器和模拟着陆面子系统,所述综控子系统、倾斜平台子系统、防护子系统和模拟着陆面子系统安装至地面上,所述防护子系统的顶部上安装测量子系统,防护子系统的中部安装起速子系统,所述起速子系统的起速拉杆通过电磁铁与模拟器的电磁铁连接件连接,实现起速子系统与模拟器之间的配合;所述模拟器的的着陆腿组件作用于倾斜平台子系统;所述模拟器的平面气垫作用于倾斜平台子系统。本发明以实现不同速度组合下、不同地形的模拟器着陆试验。
Test system for simulating low-gravity landing of moon
一种用于模拟月球低重力着陆的试验系统
2023-07-28
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |