Reduced Transversality Conditions in Optimal Space Trajectories-Reference-Cited by-同舟云学术

Reduced Transversality Conditions in Optimal Space Trajectories

Published:2013-09 Issue:5 Volume:36 Page:1289-1300
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Pan Binfeng¹,Chen Zheng¹,Lu Ping²,Gao Bo¹

Affiliation:

1. College of Astronautics, Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

2. Department of Aerospace Engineering, Iowa State University, Ames, Iowa 50011

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/10.2514/1.60181

Reference19 articles.

1. BrysonA. E.HoY. C., Applied Optimal Control, Hemisphere, Washington, DC, 1975, pp. 42–89, Chap. 2.

2. DukemanG. A., Closed-Loop Nominal and Abort Atmospheric Ascent Guidance for Rocket-Powered Launch Vehicles, Ph.D. Dissertation, Georgia Inst. of Technology, Atlanta, 2005.

3. Real-time optimal guidance

4. Optimization of Launch Vehicle Ascent Trajectories with Path Constraints and Coast Arcs

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