| 火星精确定点着陆多信息融合自主导航与控制方法研究 |
| |
| 引用本文： | 黄翔宇,徐超,胡荣海,李茂登,郭敏文,胡锦昌. 火星精确定点着陆多信息融合自主导航与控制方法研究[J]. 深空探测学报, 2019, 6(4): 348-357 |
| |
| 作者姓名： | 黄翔宇 徐超 胡荣海 李茂登 郭敏文 胡锦昌 |
| |
| 作者单位： | 北京控制工程研究所, 北京 100094;空间智能控制技术重点实验室, 北京 100094,北京控制工程研究所, 北京 100094;空间智能控制技术重点实验室, 北京 100094,北京控制工程研究所, 北京 100094;空间智能控制技术重点实验室, 北京 100094,北京控制工程研究所, 北京 100094;空间智能控制技术重点实验室, 北京 100094,北京控制工程研究所, 北京 100094;空间智能控制技术重点实验室, 北京 100094,北京控制工程研究所, 北京 100094;空间智能控制技术重点实验室, 北京 100094 |
| |
| 基金项目： | 国家自然科学基金资助项目（61673057，61803028）；民用航天预先研究资助项目 |
| |
| 摘 要： | 针对火星定点采样、载人登陆和基地构建等任务的需求,提出了一种火星精确定点着陆多信息融合自主导航与控制(Guidance Navigation and Control,GNC)方案。针对大气进入前的高精度导航需求,提出了基于X射线脉冲星和火星表面陆标图像的融合自主导航方法;针对火星着陆探测进入、下降和着陆(Entry,Descent and Landing,EDL)过程的高精度绝对和相对导航需求,提出了基于陆标图像、IMU(Inertial Measurement Unit)和测距测速信息的多信息融合自主导航方法;针对精确定点着陆要求,设计了大气进入和动力下降过程的制导与控制算法。数学仿真结果表明,提出的方案能够实现高精度的定点着陆(精度100 m)和相对避障(精度为0.5 m),可满足任务需求。
|
| 关 键 词： | 定点着陆 自主导航 信息融合 GNC方案 |
| 收稿时间： | 2019-03-31 |
| 修稿时间： | 2019-04-21 |
Research of Autonomous Navigation and Control Scheme Based on Multi-Information Fusion for Mars Pinpoint Landing |
| |
| HUANG Xiangyu,XU Chao,HU Ronghai,LI Maodeng,GUO Minwen and HU Jinchang. Research of Autonomous Navigation and Control Scheme Based on Multi-Information Fusion for Mars Pinpoint Landing[J]. Journal Of Deep Space Exploration, 2019, 6(4): 348-357 |
| |
| Authors: | HUANG Xiangyu XU Chao HU Ronghai LI Maodeng GUO Minwen HU Jinchang |
| |
| Affiliation: | Beijing Institute of Control Engineering, Beijing 100094, China;Science and Technology on Space Intelligent Control Laboratory, Beijing 100094, China,Beijing Institute of Control Engineering, Beijing 100094, China;Science and Technology on Space Intelligent Control Laboratory, Beijing 100094, China,Beijing Institute of Control Engineering, Beijing 100094, China;Science and Technology on Space Intelligent Control Laboratory, Beijing 100094, China,Beijing Institute of Control Engineering, Beijing 100094, China;Science and Technology on Space Intelligent Control Laboratory, Beijing 100094, China,Beijing Institute of Control Engineering, Beijing 100094, China;Science and Technology on Space Intelligent Control Laboratory, Beijing 100094, China and Beijing Institute of Control Engineering, Beijing 100094, China;Science and Technology on Space Intelligent Control Laboratory, Beijing 100094, China |
| |
| Abstract: | An autonomous guidance,navigation and control(GNC)scheme based on multi-information fusion is proposed for Mars pinpoint landing mission. Before entering the Mars atmosphere,an autonomous navigation scheme fusing X-Ray pulsars and Mars landmark images is employed to satisfy the requirement of high precision navigation. Then,during Mars entry,descent and landing(EDL)phase,a multi-information fusion navigation scheme is constructed for absolute and relative navigation with high precision, which consists of Mars landmark images, inertial measurement unit (IMU) and ranging and velocity sensors. With the demands of pinpoint landing, a guidance and control algorithm is also designed for Mars atmosphere entry phase and powered descent phase. Finally,numerical simulation is performed,which indicates that the landing accuracy is better than 100 m and the hazard avoidance accuracy is around 0.5 m when adopting the proposed GNC scheme. |
| |
| Keywords: | pinpoint landing autonomous navigation information fusion GNC scheme |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《深空探测学报》浏览原始摘要信息 |
|
点击此处可从《深空探测学报》下载免费的PDF全文 |
|
