| 伪卫星/惯性飞机自动着陆导引技术 |
| |
| 引用本文： | 张京娟,谢淑香,高文,冯培德.伪卫星/惯性飞机自动着陆导引技术[J].中国惯性技术学报,2005,13(5):20-23. |
| |
| 作者姓名： | 张京娟 谢淑香 高文 冯培德 |
| |
| 作者单位： | 北京航空航天大学仪器科学与光电工程学院,北京,100083 |
| |
| 摘 要： | 为进一步提高飞机精确进场着陆导引能力,减少着陆事故的发生,研究了基于伪卫星/惯性组合的自主着陆导引技术.在研究伪卫星布局与数量、时间同步等问题的基础上,利用伪卫星区域定位系统（RPS）与惯性导航组合的定位技术,不仅精度高、工作连续可靠,而且抗干扰能力强.仿真结果表明了该技术的可行性,对保障航行安全具有重要的意义.
|
| 关 键 词： | 着陆导引 RPS 伪卫星 INS |
| 文章编号： | 1005-6734(2005)05-0020-04 |
| 收稿时间： | 07 23 2005 12:00AM |
| 修稿时间： | 2005年7月23日 |
RPS/INS Guiding System for Aircraft Approaching and Landing |
| |
| ZHANG Jing-juan,XIE Shu-xiang,GAO Wen,FENG Pei-de.RPS/INS Guiding System for Aircraft Approaching and Landing[J].Journal of Chinese Inertial Technology,2005,13(5):20-23. |
| |
| Authors: | ZHANG Jing-juan XIE Shu-xiang GAO Wen FENG Pei-de |
| |
| Abstract: | An airborne RPS/INS guiding system is developed to decrease the probability of landing accident and endow it with the ability of precision approaching and landing in complicated condition. Based on the study on its geometry and synchronization, the system, with effectively integrated RPS/INS, not only has high positioning accuracy and working reliability, but also has complete independence and high anti-jamming ability. Simulation results show that it is feasible and reliable for aircraft precision approaching and landing. |
| |
| Keywords: | approaching and landing system RPS pseudo-satellite INS |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
