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Conference papers
Payload optimization for multi-stage launchers using HJB approach and application to a SSO mission
Abstract : This paper deals with a payload optimization problem for three-stage space launcher. The mission of the launch vehicle is to put the payload on a sun-synchronous (SSO) orbit. The considered flight sequence includes two boosts. The first one steers the launcher to a transfer orbit. Then, after a ballistic flight, a second boost is used to perform the orbit transfer manoeuvre to inject the payload to the targeted SSO orbit. The optimization method presented here is based on the Hamilton-Jacobi-Bellman (HJB) approach for hybrid dynamical systems.
Cited literature [16 references]
https://hal-ensta-paris.archives-ouvertes.fr//hal-01598665
Contributor : Hasnaa Zidani Connect in order to contact the contributor
Submitted on : Friday, September 29, 2017 - 6:42:51 PM
Last modification on : Tuesday, April 13, 2021 - 9:24:04 AM
Long-term archiving on: : Saturday, December 30, 2017 - 3:50:23 PM
Contributor : Hasnaa Zidani Connect in order to contact the contributor
Submitted on : Friday, September 29, 2017 - 6:42:51 PM
Last modification on : Tuesday, April 13, 2021 - 9:24:04 AM
Long-term archiving on: : Saturday, December 30, 2017 - 3:50:23 PM
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Bou-Bok-Des-Zidani.pdf
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