The invention discloses a visual aircraft flight parameter interpretation method, which comprises a data acquisition module, a data processing module, a data playback module, a flight state video reproduction module and a parameter logic judgment over-limit warning module. The data acquisition module acquires flight parameters from an aircraft flight parameter recorder and comprises a flight attitude data acquisition module, an engine parameter module, a fuel consumption data module, a hydraulic system data module and an instrument system parameter module. According to the visual aircraft flight parameter interpretation method, through comprehensive analysis of flight parameters, scientific arrangement of flight data, clarification of a flight data logic relationship, overall processing of parameters such as an engine state, a fuel system, a hydraulic system, an operating system and a flight instrument, and real playback of an aircraft flight attitude, three-dimensional viewing of the aircraft flight state is realized, and the visual aircraft flight parameter interpretation method is provided. The flight process of the aircraft is visually and truly reproduced, the interpretation work intensity of technicians on various flight parameters is greatly reduced, and the test flight work efficiency of the aircraft is improved.
本发明公开了一种可视化飞机飞行参数判读方法,包括数据采集模块、数据处理模块、数据回放模块、飞行状态视频再现模块、参数逻辑判断超限警告模块;所述数据采集模块实现从飞机飞参记录仪采集飞行参数,包括采集飞行姿态数据模块、发动机参数模块、燃油耗量数据模块、液压系统数据模块、仪表系统参数模块。该可视化飞机飞行参数判读方法通过综合分析飞行参数,科学整理飞行数据,厘清飞行数据逻辑关系,整体处理发动机状态、燃油系统、液压系统、操作系统以及飞行仪表等参数,真实回放飞机飞行姿态,实现立体观看飞机飞行状态,直观真实地再现飞机飞行过程,极大的减轻技术人员对繁多飞行参数的判读工作强度,提高了飞机试飞工作效率。
Visual aircraft flight parameter interpretation method
一种可视化飞机飞行参数判读方法
2023-02-03
Patent
Electronic Resource
Chinese
IPC: | G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / 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 |
ICAS2014_0210: APPROACHES FOR FLIGHT TESTS AIRCRAFT PARAMETER IDENTIFICATION
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