Adaptive Critic-Based Solution to an Orbit Rendezvous Problem
Recommended Citation
A. Heydari and S. N. Balakrishnan, "Adaptive Critic-Based Solution to an Orbit Rendezvous Problem," Journal of Guidance, Control, and Dynamics, vol. 37, no. 1, pp. 344 - 350, American Institute of Aeronautics and Astronautics (AIAA), Jan 2014.
The definitive version is available at https://doi.org/10.2514/1.60553
Department(s)
Mechanical and Aerospace Engineering
International Standard Serial Number (ISSN)
0731-5090
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2014 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
01 Jan 2014
