航空学报 > 2026, Vol. 47 Issue (14): 233009-233009   doi: 10.7527/S1000-6893.2025.33009

固体力学与飞行器总体设计

基于全包线型号试飞机动动作识别的飞机载荷谱编制技术

汤阿妮1(), 郭正旺1, 蒋献1, 邵妍1, 张程2, 吴浩南2   

  1. 1.中国飞行试验研究院 飞机所,西安 710089
    2.北京航空航天大学 航空科学与工程学院,北京 100191
  • 收稿日期:2025-10-30 修回日期:2025-11-24 接受日期:2025-12-08 出版日期:2025-12-29 发布日期:2025-12-25
  • 通讯作者: 汤阿妮 E-mail:tangani@sohu.com
  • 基金资助:
    国家级项目

Aircraft load spectrum compilation technology based on maneuvering action recognition of full-envelope prototype flight test

Ani TANG1(), Zhengwang GUO1, Xian JIANG1, Yan SHAO1, Cheng ZHANG2, Haonan WU2   

  1. 1.Institute of Aircraft,Chinese Flight Test Establishment,Xi’an 710089,China
    2.School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China
  • Received:2025-10-30 Revised:2025-11-24 Accepted:2025-12-08 Online:2025-12-29 Published:2025-12-25
  • Contact: Ani TANG E-mail:tangani@sohu.com
  • Supported by:
    National Level Project

摘要:

针对目前国内基于用户的专项载荷谱实测开始晚、任务剖面依据当时的训练大纲确定,不能及时给出用于全机疲劳试验的实测载荷谱,且不能随飞机实际使用情况的变化适时调整载荷谱的不足,提出基于全包线型号试飞机动动作识别的飞机载荷谱编制方法。首先根据机动动作特征参数特点,对全包线试飞数据机动动作进行识别,构建全包线机动动作数据库;其次,根据飞机设计使用情况或训练大纲确定典型任务剖面,将任务剖面分解成机动动作;第三,依据每个任务剖面机动动作组成及关键参数范围,按照等损伤原则从全包线试飞构建的机动动作库中挑选合适的动作段组合成等效任务剖面起落;最后进行载荷谱编制。该方法是在型号试飞阶段完成的全包线实测,不仅可以为全机疲劳试验及时提供可靠度更高的实测载荷谱,还可以依据飞机使用情况的变化适时调整载荷谱。

关键词: 载荷谱, 型号试飞, 全包线, 机动动作, 等损伤, 任务剖面

Abstract:

Aimed at the domestic shortcomings such as the late start of user-based special load spectrum measurement, the mission profile determined based on the training syllabus at that time, the inability to timely provide the measured load spectrum for full-aircraft fatigue testing, and the failure to adjust the load spectrum in a timely manner with changes in the actual aircraft operation conditions, this paper proposes an aircraft load spectrum compilation method based on maneuvering action recognition of full-envelope prototype flight test. Firstly, according to the characteristics of the characteristic parameters of maneuvering actions, the maneuvering actions in the full-envelope flight test data are identified, and a full-envelope maneuvering action database is constructed. Secondly, the typical mission profile is determined based on the aircraft design and operation conditions or the training syllabus, and the mission profile is decomposed into maneuvering actions. Thirdly, according to the composition of maneuvering actions and the range of key parameters in each mission profile, appropriate action segments are selected from the maneuvering action database constructed from the full-envelope flight test in accordance with the equal damage principle to form equivalent mission profile sorties. Finally, the load spectrum compilation is carried out. This method, which realizes full-envelope actual measurement during the prototype flight test phase, can not only timely provide a measured load spectrum with higher reliability for the full-aircraft fatigue test, but also adjust the load spectrum in a timely manner according to changes in the aircraft operation conditions.

Key words: load spectrum, prototype flight test, full-envelope, maneuvering action, equal damage, mission profile

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