Parametric Approach for Satellite Relative Orbit Designs and Constellations-Reference-Cited by-同舟云学术

Parametric Approach for Satellite Relative Orbit Designs and Constellations

Published:2021-03 Issue:3 Volume:44 Page:488-492
ISSN:1533-3884
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Lee Soung Sub¹,Hall Christopher D.²

Affiliation:

1. Department of Space Development Division, Republic of Korea Air Force 663, Chungcheongnam-do, 32820 Korea

2. University of New Mexico, Albuquerque, New Mexico 87131

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

Reference6 articles.

1. WertzJ. R., Mission Geometry: Orbit and Constellation Design and Management, Microcosm, Inc., El Segundo, CA, 2001, pp. 522–525.

2. LeeS. S. “Dynamics and Control of Satellite Relative Motion: Designs and Applications,” Ph.D. Thesis, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 2009.

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4. Correction: Parametric Approach for Satellite Relative Orbit Designs and Constellations;Journal of Guidance, Control, and Dynamics;2021-04