Three-Dimensional Optimum Thrust Trajectories for Power Limited Propulsion Systems-Reference-Cited by-同舟云学术

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Three-Dimensional Optimum Thrust Trajectories for Power Limited Propulsion Systems

Published:1961-12 Issue:12 Volume:31 Page:1723-1728
ISSN:1936-9972
Container-title:ARS Journal
language:en
Short-container-title:ARS Journal

Author:

MELBOURNE WILLIAM G.¹

Affiliation:

1. Jet Propulsion Laboratory, Pasadena, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.5902

Reference3 articles.

1. Melbourne, W. G. "Interplanetary Trajectories and Payload Capabilities of Advanced Propulsion Vehicles," Tech. Rep. no. 32-68, Jet Propulsion Laboratory, Pasadena, Calif., 1961.

2. Melbourne, W. G. and Sauer, C. G., Jr. "Optimum Thrust Programs for Power-Limited Propulsion Systems," Tech. Rep. no. 82-118, Jet Propulsion Laboratory, Pasadena, Calif., 1961.

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1. Finding analytic solutions on active arcs of the optimal trajectory in a gravitational field and their applications;Automation and Remote Control;2017-02

2. Optimum low-thrust rendezvous and station keeping;J SPACECRAFT ROCKETS;2003

3. Orbital Maneuvers via Feedback Linearization and Bang-Bang Control;Journal of Guidance, Control, and Dynamics;1997-01

4. Optimal power-limited rendezvous with upper and lower bounds on thrust;Journal of Guidance, Control, and Dynamics;1996-09

5. Optimal power-limited rendezvous of a spacecraft with bounded thrust and general linear equations of motion;Journal of Optimization Theory and Applications;1995-12

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