Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Eric Joffre"'
Publikováno v:
Acta Astronautica. 190:118-133
STORM is a general semi-analytical propagation code developed at Airbus Defence and Space and originally designed to perform long-term Mars orbit simulations, for mission analysis purposes. Since the 1960’s, humans have sent 18 spacecraft to study
Autor:
Ignacio Fernandez, Philipp Voigt, Dave Wealthy, Waldemar Martens, Tobias Ziegler, Eric Joffre, Christian Trenkel
Publikováno v:
Advances in Space Research. 67:3868-3879
The LISA (Laser Interferometer Space Antenna) mission has been selected by the European Space Agency’s Science Programme Committee as the third large-class mission of the Cosmic Vision Programme, addressing the science theme of the Gravitational Un
Publikováno v:
Simplicio, P, Marcos, A, Joffre, E, Zamaro, M & Silva, N 2019, ' Systematic performance-oriented guidance tuning for descent & landing on small planetary bodies ', Acta Astronautica, vol. 158, pp. 44-54 . https://doi.org/10.1016/j.actaastro.2018.07.028
Descent & landing (D&L) on small planetary bodies are scientifically rewarding exploration missions but they are technically challenging due to the complex and poorly-known environment around those bodies. The standard guidance synthesis approach con
Autor:
Waldemar Martens, Eric Joffre
The three Laser Interferometer Space Antenna (LISA) spacecraft are going to be placed in a triangular formation in an Earth-trailing or Earth-leading orbit. They will be launched together on a single rocket and transferred to that science orbit using
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1c12769c3da5288e1f0cdd3391826581
Publikováno v:
International Journal of Robust and Nonlinear Control. 28:3871-3892
Publikováno v:
Simplicio, P, Marcos, A, Joffre, E, Zamaro, M & Silva, N 2018, Robust Control Compensation for Space Descent and Landing . in 2018 European Control Conference (ECC 2018) : Proceedings of a meeting held 12-15 June 2018, Limassol, Cyprus . Institute of Electrical and Electronics Engineers (IEEE), pp. 155-160, 17th European Control Conference, 12/06/18 . https://doi.org/10.23919/ECC.2018.8550147
ECC
ECC
This paper presents a complete modelling, synthesis and analysis methodology of control compensators for descent and landing on small planetary bodies. These missions are scientifically very rewarding, but also extremely challenging due to the comple
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1c7601fd1821b5fb147e277580d63c6b
https://research-information.bris.ac.uk/en/publications/36c1bd9b-f1e1-41af-8684-53ab81935f27
https://research-information.bris.ac.uk/en/publications/36c1bd9b-f1e1-41af-8684-53ab81935f27
Publikováno v:
Simplicio, P, Marcos, A, Joffre, E, Zamaro, M & Silva, N 2018, ' Review of guidance techniques for landing on small bodies ', Progress in Aerospace Sciences, vol. 103, pp. 69-83 . https://doi.org/10.1016/j.paerosci.2018.10.005
A renewed scientific interest has been growing in the exploration of small asteroids in addition to larger planetary bodies such as Mars, since their weaker gravitational field makes them more easily accessible. However, such exploratory missions are
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1c5aa70c1490ce39d97a37709496e47e
https://research-information.bris.ac.uk/ws/files/174314544/PAS_Review_of_Guidance_Techniques_for_Landing_on_Small_Bodies_Preprint.pdf
https://research-information.bris.ac.uk/ws/files/174314544/PAS_Review_of_Guidance_Techniques_for_Landing_on_Small_Bodies_Preprint.pdf
Publikováno v:
Joffre, E, Zamaro, M, Silva, N, Marcos, A & Simplício, P 2018, ' Trajectory design and guidance for landing on Phobos ', Acta Astronautica, vol. 151, pp. 389-400 . https://doi.org/10.1016/j.actaastro.2018.06.024
While common Descent and Landing strategies involve extended periods of forced motion, significant fuel savings could be achieved by exploiting the natural dynamics in the vicinity of the target. However, small bodies are characterised by perturbed a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::422b488080c9a754b9f2535cafa6ad88
https://hdl.handle.net/1983/2850f1ff-c2fb-4847-8f59-7ca7073fce03
https://hdl.handle.net/1983/2850f1ff-c2fb-4847-8f59-7ca7073fce03
Publikováno v:
Joffre, E, Zamaro, M, Silva, N, Marcos, A, Simplício, P & Richardson, B 2017, Landing on small bodies trajectory design, robust nonlinear guidance and control . in Spaceflight Mechanics 2017 . vol. 160, AAS 17-370, Univelt Inc., pp. 1425-1444, 27th AAS/AIAA Space Flight Mechanics Meeting, 2017, San Antonio, United States, 5/02/17 . < http://www.univelt.com/book=6135 >
University of Bristol-PURE
Scopus-Elsevier
University of Bristol-PURE
Scopus-Elsevier
While common Descent and Landing strategies involve extended periods of forced motion, significant fuel savings could be achieved by exploiting the natural dynamics in the vicinity of the target. However, small bodies are characterized by perturbed a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::b8d7dd225871dfbcb25e5b2ba15aa4b2
https://hdl.handle.net/1983/c3fed4bc-44c7-40b0-9133-b3aca0ac7dcc
https://hdl.handle.net/1983/c3fed4bc-44c7-40b0-9133-b3aca0ac7dcc
Autor:
Aurélien Pisseloup, Nimal Navarathinam, Jason L. Forshaw, Haval Kadhem, Andrew Ratcliffe, Eric Joffre, Robert Axthelm, Alexandre Pollini, François Chaumette, Cesar Bernal, Thomas Chabot, Guglielmo S. Aglietti, Willem H. Steyn, Thierry Salmon, Simon Barraclough, Ingo Retat
Publikováno v:
Acta Astronautica
Acta Astronautica, 2016, 127, pp.448-463. ⟨10.1016/j.actaastro.2016.06.018⟩
Acta Astronautica, Elsevier, 2016, 127, pp.448-463. ⟨10.1016/j.actaastro.2016.06.018⟩
Acta Astronautica, 2016, 127, pp.448-463. ⟨10.1016/j.actaastro.2016.06.018⟩
Acta Astronautica, Elsevier, 2016, 127, pp.448-463. ⟨10.1016/j.actaastro.2016.06.018⟩
International audience; Since the beginning of the space era, a significant amount of debris has progressively been generated. Most of the objects launched into space are still orbiting the Earth and today these objects represent a threat as the pres
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ef8415f6cd544331ab45871a82d65a55
https://hal.inria.fr/hal-01342268
https://hal.inria.fr/hal-01342268