| 舰载飞机着舰精确轨迹控制研究 |
| |
| 引用本文： | 张勇,张东光.舰载飞机着舰精确轨迹控制研究[J].飞机设计,2006(1):50-55. |
| |
| 作者姓名： | 张勇 张东光 |
| |
| 作者单位： | 沈阳飞机设计研究所,辽宁,沈阳,110035 |
| |
| 摘 要： | 针对舰载机着舰过程的精确航迹控制要求,利用现有机上的控制设备,采用系统综合设计的方法,给出了两种航迹控制系统———风参考航迹控制系统和惯性参考航迹控制系统,通过仿真分析,给出了系统的性能差异。
|
| 关 键 词： | 舰载机 航迹控制系统 增稳系统 进场动力补偿 直接力飞行控制 |
| 文章编号： | 1673-4599（2006）01-0050-06 |
| 收稿时间： | 2005-07-16 |
| 修稿时间： | 2005年7月16日 |
Precision Flight Path Control for Carrier - Based Aircraft Landing Approaches |
| |
| ZHANG Yong,ZHANG Dong-guang.Precision Flight Path Control for Carrier - Based Aircraft Landing Approaches[J].Aircraft Design,2006(1):50-55. |
| |
| Authors: | ZHANG Yong ZHANG Dong-guang |
| |
| Abstract: | Based on the requirements for precision flight path control during the carrier-based aircraft oncarrier landing approach,two different flight path control systemswind-referenced flight path control system and inertia-referenced flight path control system-are designed by means of a system integration design approach,utilizing existing flight control effectors.Performance differences in between the two systems are identified by system simulation. |
| |
| Keywords: | carrier-based aircraft flight path control system stability augmentation system approach power compensation direct lift control |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
