Design and Simulation of Discrete Gust Load for T-Tail Aircraft Considering Control Law

被引：0
|
作者：
Liu, Xiaochen [1 ]
Yan, Zhongwu [1 ]
机构：
[1] Shanghai Aircraft Design & Res Inst, Shanghai 201210, Peoples R China
来源：
2023 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL I, APISAT 2023 | 2024年 / 1050卷
关键词：
T-tail; Gust gradient; Gust load; Control law;
D O I：
10.1007/978-981-97-3998-1_64
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this article, a batch simulation platform for gust loads based on terms and scenario requirements was established, by which the gust loads of a T-tail aircraft under different conditions and inputs were analyzed and compared. The research showed that there were certain differences in the calculation results of gust loads with and without considering control laws, which were related to the logic of the transfer function. On the other hand, there were certain rules in the calculation results under different input parameters of gust loads. By early variable parameter analysis, we could fully consider various calculation scenarios and working conditions as well as improve the calculation and evaluation efficiency between different rounds.
引用
收藏
页码：768 / 776
页数：9
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