Along-Track Boundedness Condition for Spacecraft Relative Motion Around a Slowly Rotating Asteroid-Reference-Cited by-同舟云学术

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Along-Track Boundedness Condition for Spacecraft Relative Motion Around a Slowly Rotating Asteroid

Published:2023-02 Issue:1 Volume:59 Page:497-506
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Wang Wei¹^ORCID,Lei Hanlun²,Mengali Giovanni³^ORCID,Quarta Alessandro A.³^ORCID,Baoyin Hexi⁴^ORCID

Affiliation:

1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai, China

2. School of Astronomy and Space Science, Nanjing University, Nanjing, China

3. Department of Civil and Industrial Engineering, University of Pisa, Pisa, Italy

4. School of Aerospace Engineering, Tsinghua University, Beijing, China

Funder

National Natural Science Foundation of China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

http://xplorestaging.ieee.org/ielx7/7/10041225/09796581.pdf?arnumber=9796581

Reference33 articles.

1. Bounded Satellite Relative Motion in Coplanar Three-Body Systems

2. Analytical Conditions for Bounded Mean Inter-Satellite Distances in the J2 Problem

3. Improved initialization conditions and single impulsive maneuvers for $$\hbox {J}_{2}$$ J 2 -invariant relative orbits

4. Precise Determination of Reachable Domain for Spacecraft with Single Impulse

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1. Spacecraft Relative Motion Control Near an Asteroid With Uncertainties: A Lyapunov Redesign Approach;IEEE Transactions on Aerospace and Electronic Systems;2024-08

2. A framework of gravity field online modeling and trajectory optimization in asteroid soft-landing mission scenarios;Aerospace Science and Technology;2023-12

3. Design of Mars global longitudinal coverage constellation leveraging resonant and periodic orbits in Mars-Phobos-Deimos system;Advances in Space Research;2023-07

4. Optimal Projected Circular Orbit for Spacecraft Formation Flying Near a Slowly Rotating Asteroid;IEEE Transactions on Aerospace and Electronic Systems;2022-12

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