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| 跨大气层飞行器爬升段飞行控制律方案研究 | |
| 引用本文： | 周欲晓,张子彦,明晓.跨大气层飞行器爬升段飞行控制律方案研究[J].飞行力学,2006,24(1):9-12. |
| 作者姓名： | 周欲晓 张子彦 明晓 |
| 作者单位： | 1. 南京航空航天大学,无人机研究所,江苏,南京,210016 2. 成都飞机设计研究所,四川,成都,610041 3. 南京航空航天大学,宇航学院,江苏,南京,210016 |
| 摘 要： | 跨大气层飞行器在爬升过程中重量、重心、高度和速度等参数变化剧烈,因而飞行器的操纵稳定特性也变化急剧,与常规飞行器相比其飞行控制律设计有它的特殊性。针对跨大气层飞行器的飞行特点,提出了四种纵向控制律初步方案,分析研究了这四种控制律设计方案的特点及存在问题,为具体的控制律方案设计提供了初步基础。 |
| 关 键 词： | 跨大气层飞行器 爬升段 控制律 设计方案 |
| 文章编号： | 1002-0853（2006）01-0009-04 |
| 收稿时间： | 2004-10-25 |
| 修稿时间： | 2004-10-252005-12-14 |
Conceptual Study on Flight Control Laws for a Trans-Aerosphere Vehicle in Climbing Phase |
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| ZHOU Yu-xiao,ZHANG Zi-yan,MING Xiao.Conceptual Study on Flight Control Laws for a Trans-Aerosphere Vehicle in Climbing Phase[J].Flight Dynamics,2006,24(1):9-12. | |
| Authors: | ZHOU Yu-xiao ZHANG Zi-yan MING Xiao |
| Institution: | 1. Research Institute of Unmanned Vehicle, NUAA, Nanjing 210016, China; 2. Chengdu Aircraft Design and Research Institute, Chengdu 610041, China; 3. Aerospace Institute, NUAA, Nanjing 210016, China |
| Abstract: | During the climbing phase,the parameters,such as weight,center of weight,altitude and velocity of a trans-aerosphere vehicle changed so much so that its control and stability also change so much.Based on the flight characteristics of the trans-aerosphere vehicle,the preliminary schemes for control systems were presented.A better one was selected by analyzing several inner and outer loops projects. |
| Keywords: | trans-aerosphere vehicle climbing phase control system project design |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |