Optimal Satellite-Formation Collision-Avoidance Maneuver Based on Relative E/I Vectors-Reference-Cited by-同舟云学术

Optimal Satellite-Formation Collision-Avoidance Maneuver Based on Relative E/I Vectors

Published:2016-11 Issue:6 Volume:29 Page:04016048
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Shao Xiaowei¹,Wang Jihe²,Zhang Dexin³,Chen Junli⁴

Affiliation:

1. Associate Professor, School of Aeronautics and Astronautics, Shanghai Jiao Tong Univ., 800 Dong Chuan Rd., Min Hang District, Shanghai 200240, China (corresponding author).

2. Researcher, School of Aeronautics and Astronautics, Shanghai Jiao Tong Univ., 800 Dong Chuan Rd., Min Hang District, Shanghai 200240, China.

3. Lecturer, School of Aeronautics and Astronautics, Shanghai Jiao Tong Univ., 800 Dong Chuan Rd., Min Hang District, Shanghai 200240, China.

4. Postdoctor, School of Aeronautics and Astronautics, Shanghai Jiao Tong Univ., 800 Dong Chuan Rd., Min Hang District, Shanghai 200240, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000642

Reference11 articles.

1. GPS-based relative navigation for the Proba-3 formation flying mission

2. Spaceborne Autonomous Formation-Flying Experiment on the PRISMA Mission

3. Proximity Operations of Formation-Flying Spacecraft Using an Eccentricity/Inclination Vector Separation

4. Impulsive Maneuvers for Formation Reconfiguration Using Relative Orbital Elements

5. Larsson R. Mueller J. Thomas S. Jakobsson B. and Bodin P. (2008). “Orbit constellation safety on the PRISMA in-orbit formation flying testbed.” 3rd Int. Symp. on Formation Flying Missions and Technologies European Space Agency Noordwijk Netherlands.

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