Autonomous navigation and guidance for landing on asteroids

Li Shuang; Cui Pingyuan; Cui Hutao

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Autonomous navigation and guidance for landing on asteroids

机译：自主导航和登陆小行星的指导

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摘要

This paper presents an autonomous landing navigation and guidance scheme for future asteroid sample return mission. An autonomous navigation scheme based on feature tracking technology is brought out firstly; secondly, desired descent landing trajectories with the initial and terminal constraints are planned in order to achieve arrive-at-time landing on an asteroid; then, two guidance control laws, based on error phase analysis method and PD plus PWPF method respectively, are designed to track reference descent trajectory; finally, the validity of the proposed scheme is confirmed by computer simulation.

机译：本文提出了未来小行星样本返回任务的自主着陆导航和制导方案。首先提出了一种基于特征跟踪技术的自主导航方案。其次，计划在初始和最终约束条件下的理想下降着陆轨迹，以实现在小行星上的及时到达着陆。然后，分别基于误差相位分析法和PD加PWPF法，设计了两种制导控制律来跟踪参考下降轨迹。最后，通过计算机仿真验证了所提方案的有效性。

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来源
《Aerospace science and technology》 |2006年第3期|p.239-247|共9页
作者
Li Shuang; Cui Pingyuan; Cui Hutao;
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作者单位

Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin, 150001, China;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空、航天;
关键词
autonomous landing; navigation and guidance; feature tracking; error phase analysis; PWPf;

机译：自主着陆;导航与制导;特征跟踪;误差阶段分析;PWPf;

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专利

1. Erratum to 'Autonomous navigation and guidance for landing on asteroids' [Aerospace Science and Technology 10 (2006) 239-247] [J] . Li Shuang, Cui Pingyuan, Cui Hutao Aerospace science and technology . 2008,第5期

机译：对“在小行星上着陆的自主导航和制导”的勘误表[航空科学与技术10（2006）239-247]
2. An autonomous optical navigation and guidance for soft landing on asteroids [J] . Huang Xiangyu, Cui Hutao, Cui Pingyuan Acta astronautica . 2004,第10期

机译：自主光学导航和制导，可在小行星上软着陆
3. An autonomous navigation and guidance system for MUSES-C asteroid landing [J] . Takashi Kubota, Tatsuaki Hashimoto, Shujiro Sawai, Acta astronautica . 2003,第2a6期

机译：用于MUSES-C小行星着陆的自主导航和制导系统
4. A method of guidance, navigation and control for soft landing on asteroid based on constrained MPC [C] . Wei Ruoyan, Ruan Xiaogang, Zhu Xiaoqing, World Congress on Intelligent Control and Automation . 2014

机译：基于约束MPC的小行星软着陆的制导，导航和控制方法
5. Entry Guidance and Navigation for High Elevation Mars Landing [D] . Duan, Guangfei. 2019

机译：高海拔火星着陆的入门指导和导航
6. A Computationally Inexpensive Optimal Guidance via Radial-Basis-Function Neural Network for Autonomous Soft Landing on Asteroids [O] . Peng Zhang, Keping Liu, Bo Zhao, -1

机译：通过径向基函数神经网络的计算廉价最优制导用于小行星自主软着陆
7. A Predictive Guidance Algorithm for Autonomous Asteroid Soft Landing [O] . Julio C. Sanchez, Francisco Gavilan, Rafael Vazquez 2018

机译：一种自主小行星软着陆预测指导算法

Autonomous navigation and guidance for landing on asteroids

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