Research on Asteroid Landing with a New Flexible Spacecraft-Reference-Cited by-同舟云学术

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Research on Asteroid Landing with a New Flexible Spacecraft

Published:2022-09 Issue:5 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhai Guang¹,Li Jie²,Sun Yiyong³,Zheng Heming⁴^ORCID

Affiliation:

1. Professor, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.

2. Graduate Student, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.

3. Assistant Professor, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China (corresponding author).

4. Ph.D. Student, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001466

Reference36 articles.

1. Soft landing on an irregular shape asteroid using Multiple-Horizon Multiple-Model Predictive Control

2. Direct Trajectory Optimization and Costate Estimation via an Orthogonal Collocation Method

3. The Philae lander mission and science overview

4. Fast Generation of Optimal Asteroid Landing Trajectories Using Deep Neural Networks

5. Optimal commands based multi-stage drag de-orbit design for a tethered system during large space debris removal

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Concurrent learning-based trajectory tracking control of a novel multi-node flexible lander for asteroid missions;Aircraft Engineering and Aerospace Technology;2024-08-28

2. Controllable cone for horizontal landing on asteroids using a flexible probe;Aerospace Science and Technology;2024-02

3. Modeling ＆ Control for a Novel Multi-node Flexible Asteroid Lander Based on Port-Hamilton Framework;Space: Science & Technology;2023-12-12

4. Position-attitude coupling guidance and control for asteroid landing with a flexible lander;Aerospace Science and Technology;2023-10

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