Rendezvous Trajectory Control Laws in Low Earth Orbit Using Neural ODE for Continuous System Deep Learning
Author:
Affiliation:
1. Research and Development Directorate, Japan Aerospace Exploration Agency
2. Graduate School of Engineering, Kyushu University
Publisher
The Society of Instrument and Control Engineers
Link
https://www.jstage.jst.go.jp/article/sicetr/60/3/60_218/_pdf
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3. 3) A.R. Klumpp: Apollo lunar descent guidance, Automatica, 10-2, 133/146 (1974)
4. 4) O. von Stryk and R. Bulirsch: Direct and indirect methods for trajectory optimization, Annals of Operations Research, 37, 357/373 (1992)
5. 5) L.S. Pontryagin, E.F. Mishchenko, V.G. Boltyanskii and R.V. Gamkrelidze: The Mathematical Theory of Optimal Processes, CRC Press (1962)
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