Optimization of the launcher ascent trajectory leading to the global optimum without any initialization: the breakthrough of the HJB approach
2018
Publication type:
International conference with proceedings
Journal:
EUCASS Proceedings "Progress in Flight Dynamics, Guidance, Navigation, and Control",, vol. 10, pp. 159-176
Conference:
Selected paper at the "6th European Conference for Aeronautics and Space Sciences - EUCASS", June 2015, Kraków, Poland.
HAL:
BibTeX:
@inproceedings{Bou-Bok-Des-Zid-2018, author={Eric Bourgeois and Olivier Bokanowski and Anna Désilles and Hasnaa Zidani }, title={Optimization of the launcher ascent trajectory leading to the global optimum without any initialization: the breakthrough of the HJB approach }, doi={10.1051/eucass/201810159 }, organization={Selected paper at the "6th European Conference for Aeronautics and Space Sciences - EUCASS", June 2015, Kraków, Poland. }, booktitle={EUCASS Proceedings "Progress in Flight Dynamics, Guidance, Navigation, and Control", }, year={2018 }, volume={10 }, pages={159--176}, }