Multiple-Spacecraft Orbit-Transfer Problem: The No-Booster Case-Reference-Cited by-同舟云学术

Multiple-Spacecraft Orbit-Transfer Problem: The No-Booster Case

Published:1999-09 Issue:5 Volume:22 Page:650-657
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Ocampo Cesar A.¹,Rosborough George W.¹

Affiliation:

1. University of Colorado, Boulder, Colorado 80309

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

http://arc.aiaa.org/doi/pdf/10.2514/2.4453

Reference14 articles.

1. Optimal cooperative time-fixed impulsive rendezvous

2. Ocampo, C. A. “Trajectory Optimization for Distant Earth Satellites and Satellite Constellations,” Ph.D. Dissertation, Dept. of Aerospace Engineering Sciences, Univ. of Colorado, Boulder, CO,Aug. 1996; University Microfilms Inc. (UMI), Publ. 9709513, Ann Arbor, MI.

3. Description of the Restricted Problem

4. Battin, R. H., An Introduction to the Mathematics and Methods of Astrodynamics, AIAA Education Series, AIAA, New York, 1987, pp.450- 454.

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