| 廖智麟, 陆晓安, 黄一敏, 甄子洋.直升机着舰引导与控制研究进展[J].南京航空航天大学学报,2018,50(6):745-753 |
| 直升机着舰引导与控制研究进展 |
| Research Progress of Landing Guidance and Control for Carrier-Based Helicopter |
| 投稿时间：2018-09-27 修订日期：2018-11-10 |
| DOI：10.16356/j.1005-2615.2018.06.003 |
| 中文关键词: 直升机 着舰引导 着舰控制 自动着舰 |
| 英文关键词:helicopter landing guidance landing control automatic boarding |
| 基金项目:国家自然科学基金（61533008）资助项目。 |
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| 摘要点击次数: 1993 |
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| 中文摘要: |
| 随着现代海战向立体化、多层化发展，舰载直升机以其垂直起降、定点悬停等优势成为未来海战武器装备的重要组成部分，而着舰引导与控制是舰载直升机的关键技术。本文对直升机着舰引导技术与着舰控制技术的研究进展进行概述，着重概述和分析了着舰引导技术中的雷达、卫星、视觉、光电引导技术。其次对舰载直升机着舰的环境影响因素、综合流程以及应用现状进行概述分析，最后对舰载直升机着舰技术进行了展望。 |
| 英文摘要: |
| With the three-dimensional and multi-layered development of modern naval warfare, carrier-based helicopter has become an increasingly important part of future naval warfare with its advantages of vertical takeoff and landing and fixed-point hovering. Landing guidance and control is the key technology of carrier-based helicopter. In this paper, the research progress of helicopter landing guidance technology and control technology is described, in which the radar, satellite, vision and photoelectric guidance techniques are emphatically described. Moreover, the landing environments, general process and applications are summarized. Finally, the future of helicopter carrier landing technology is explained. |
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