[1]夏桂华,董然,孟雪,等.舰载机着舰的动力学建模[J].哈尔滨工程大学学报,2014,(04):445-456.[doi:10.3969/j.issn.10067043.201309033]
 XIA Guihua,DONG Ran,MENG Xue,et al.Research on the dynamic modeling for the landing of a carrierbased aircraft[J].hebgcdxxb,2014,(04):445-456.[doi:10.3969/j.issn.10067043.201309033]
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舰载机着舰的动力学建模(/HTML)
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《哈尔滨工程大学学报》[ISSN:1006-6977/CN:61-1281/TN]

卷:
期数:
2014年04期
页码:
445-456
栏目:
出版日期:
2014-04-25

文章信息/Info

Title:
Research on the dynamic modeling for the landing of a carrierbased aircraft
文章编号:
10067043(2014)04044512
作者:
夏桂华 董然 孟雪 朱齐丹
哈尔滨工程大学 自动化学院,黑龙江 哈尔滨 150001
Author(s):
XIA GuihuaDONG RanMENG XueZHU Qidan
College of Automation, Harbin Engineering University, Harbin 150001, China
关键词:
舰载机6自由度运动方程基准状态配平扰动线性化舰尾气流场动力学模型
分类号:
V212.12
DOI:
10.3969/j.issn.10067043.201309033
文献标志码:
A
摘要:
为了实现舰载机精确着舰时的飞行控制系统设计,应具备完善的舰载机动力学模型。针对已公开的线性扰动模型较为单一且多数不完整的情况,根据舰载机的性能参数和标准小扰动理论,完成了对其着舰阶段的非线性动力学建模,基准状态配平以及纵向运动的线性化,得到能描述舰载机在平静大气和舰尾气流场下着舰的线性模型。根据舰载机的本体特性综合设置数值仿真条件,验证表明线性模型的精度较高。分析了将气流扰动加入线性模型的方法,通过理论分析和仿真比较得出,舰尾流的水平速度分量对线性模型的精度有很大影响,在扰动线性化的过程中不能忽视。

参考文献/References:

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备注/Memo

备注/Memo:
收稿日期: 2013-09-09. 网络出版时间:2014-03-15 20:43:38. 基金项目:国家自然科学基金资助项目(61104037,11372080);中央 高校基金资助项目(HEUCF041307);国家科技合作专项资 助项目(2013DFR10030). 作者简介:夏桂华(1962-), 男, 教授, 博士生导师; 董然(1987-), 男, 博士研究生. 通信作者:董然, E-mail: dongran@ hrbeu.edu.cn.
更新日期/Last Update: 2014-07-07