Optimal Analytic Multiburn Trajectories
Author:
Affiliation:
1. NASA Manned Spacecraft Center, Houston, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50176
Reference14 articles.
1. Variational Problems with Bounded Control Variables
2. Quasilinearization determination of optimum finite-thrust orbital transfers.
3. Kern, E. A. "Minimum-Fuel Thrust-Limited Transfer Trajectories Between Coplanar Elliptic Orbits," Ph.D. thesis,1968, Univ. of Michigan, Ann Arbor, Midi.
4. Rocket trajectory optimization by a second- order numerical technique.
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