Minimum-Fuel Finite-Thrust Relative Orbit Maneuvers via Indirect Heuristic Method-Reference-Cited by-同舟云学术

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Minimum-Fuel Finite-Thrust Relative Orbit Maneuvers via Indirect Heuristic Method

Published:2015-05 Issue:5 Volume:38 Page:913-924
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Pontani Mauro¹,Conway Bruce A.¹

Affiliation:

1. University “La Sapienza”, University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

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/10.2514/1.G000157

Reference33 articles.

1. LawdenD. F., Optimal Trajectories for Space Navigation, Butterworths, London, 1963, pp. 30–124.

2. Variational Problems with Bounded Control Variables

3. EdelbaumT. N. “Optimal Space Trajectories,” Analytical Mechanics Associates, Rept. 69-4, Hampton, VA, 1969.

4. MarecJ. P., Optimal Space Trajectories, Elsevier, New York, 1979, pp. 53–70.

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