Trajectory optimization using regularized variables.-Reference-Cited by-同舟云学术

Trajectory optimization using regularized variables.

Published:1969-06 Issue:6 Volume:7 Page:1010-1017
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

TAPLEY B. D.¹,SZEBEHELY V.¹,LEWALLEN J. M.²

Affiliation:

1. The University of Texas at Austin, Austin, Texas

2. NASA Manned Spacecraft Center, Houston, Texas

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.5268

Reference10 articles.

1. Presented as AAS Paper 68-099 at the AAS/AIAA Astrodynamics Specialist Conference, Jackson, Wyo., September3-5, 1968; submitted December 4,1968. The investigation leading to the results presented here was initiated at the Jet Propulsion Laboratory during the summer of1967. The subsequent study was supported by NASA under NGR-012-046 and NAS9-6963.

2. Comparison of several numerical optimization methods

3. A Group of Earth-to-Moon Trajectories with Consecutive Collisions

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