Determination of Dynamic Load Condition of Aircraft Carrier based on Multivariable Distribution of Flight Parameters

• 作者: JIN Xin LIU Yu ZHANG Jian'gang
• 来源期刊: 国际设备工程与管理（英文版）
• 年，卷（期）: 2020,（4）
• 页码范围: 223-237
• 页数: 15页
• 语种: 英文
• DOI: 10.13434/j.cnki.1007-4546.2020.0403

摘要

In order to solve the design problem of dynamic load of a carrier-based aircraft, accordingto the relevant criteria of national military standards, eight key flight parameters of the dynamic load conditions for the aircraft carrier were selected. Based on the multivariable distribution data of landing flight parameters obtained from flight test, the distribution form and range limitation of each flight parameter were determined by using the probability distribution of each flight parameter and the spatial relationship among variables. Furthermore, 100000 sets of data were constructed to simulate the landing condition of aircraft in the form of random number. After the envelope is screened by multivariable joint probability distribution, the boundary conditions were compared and merged, and finally the dynamic load conditions were obtained. In this paper, a set of dynamic load condition design method based on the aircraft requirements is constructed, which systematically covers all kinds of situations that occur in the process of aircraft landing, and improves the conventional design process of aircraft dynamic load.