The invention belongs to the technical field of aircraft ground tests, and relates to an aircraft ground test system, which comprises a main control device, an external test device and/or an internal test device, and is characterized in that the main control device is connected with the external test device and/or the internal test device; the master control device is used for collecting data and processing the data to realize system master control, information storage interaction, module communication and unified time reference; the external testing device is used for acquiring relative position information, infrared information, time information and speed information of the aircraft; the internal testing device is used for collecting mechanical information, pressure information, angle information and parameter information of the aircraft and carrying out multi-channel information management and aircraft control. According to the invention, data can be comprehensively and completely collected, and full-size aircraft ground tests can be carried out.
本申请属于飞行器地面试验技术领域,涉及一种飞行器地面试验系统,包括:主控装置、外测试装置和/或内测试装置,主控装置与外测试装置和/或内测试装置相连;主控装置用于采集数据进行处理以实现系统主控、信息存储交互、模块通信以及统一时间基准;外测试装置用于采集飞行器的相对位置信息、红外信息、时刻信息以及速度信息;内测试装置用于采集飞行器的力学信息、压力信息、角度信息和参数信息,并进行多通道信息管理和飞行器控制。采用本申请能够全面完整采集数据并能够进行全尺寸的飞行器地面试验。
Aircraft ground test system
一种飞行器地面试验系统
2024-06-14
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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