Reformulation of Edelbaum's Low-Thrust Transfer Problem Using Optimal Control Theory-Reference-Cited by-同舟云学术

Reformulation of Edelbaum's Low-Thrust Transfer Problem Using Optimal Control Theory

Published:1997-09 Issue:5 Volume:20 Page:988-994
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Kechichian Jean Albert¹

Affiliation:

1. The Aerospace Corporation, El Segundo, California 90245-4691

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/10.2514/2.4145

Reference12 articles.

1. Propulsion Requirements for Controllable Satellites

2. Theory of Maxima and Minima

3. Cass, J. R. “Discontinuous Low Thrust Orbit Transfer,” M.S. Thesis, School of Engineering,Air ForceInst. of Technology, AFIT/GA/AA/83D-1, Wright-Patterson AFB,OH, Dec. 1983.

4. McCann, J. M. “Optimal Launch Time for a Discontinuous Low Thrust Orbit Transfer,” M.S. Thesis, School of Engineering,Air ForceInst. of Technology, AFIT/GA/AA/88D-7, Wright-Patterson AFB,OH, Dec. 1988.

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