Hybrid Differential Dynamic Programming in the Circular Restricted Three-Body Problem
Author:
Affiliation:
1. University of Colorado Boulder, Boulder, Colorado 80309
2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
Funder
National Aeronautics and Space Administration
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
https://arc.aiaa.org/doi/am-pdf/10.2514/1.G003617
Reference25 articles.
1. A Second-order Gradient Method for Determining Optimal Trajectories of Non-linear Discrete-time Systems
2. A discrete-time differential dynamic programming algorithm with application to optimal orbit transfer
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