Fuel-Optimal Spacecraft Cluster Flight Around an Ellipsoidal Asteroid-Reference-Cited by-同舟云学术

Fuel-Optimal Spacecraft Cluster Flight Around an Ellipsoidal Asteroid

Published:2021-10 Issue:10 Volume:44 Page:1875-1882
ISSN:1533-3884
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Wang Wei¹,Wu Di²,Lei Hanlun³,Baoyin Hexi²

Affiliation:

1. Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China

2. Tsinghua University, 100084 Beijing, People’s Republic of China

3. Nanjing University, 210023 Nanjing, People’s Republic of China

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G005993

Reference35 articles.

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2. Electric Sail for a Near-Earth Asteroid Sample Return Mission: Case 1998 KY26

3. Rapid Solar Sail Rendezvous Missions to Asteroid 99942 Apophis

4. An artificial impact on the asteroid (162173) Ryugu formed a crater in the gravity-dominated regime

5. NASA's swarm missions: the challenge of building autonomous software

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