An analytic solution for constant-thrust, optimal-coast, minimum-propellant space trajectories
Author:
Affiliation:
1. University of Minnesota, Minneapolis, Minn.
2. Princeton University, Princeton, N. J.
3. Convair Division of General Dynamics, San Diego, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6347
Reference12 articles.
1. Analytical determination of the adjoint vector for optimum space trajectories
2. Constants of the motion for optimum thrust trajectories in a central force field
3. Optimal free-space fixed-thrust trajectories using impulsive trajectories as starting iteratives.
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