Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Leandro R. Lustosa"'
Publikováno v:
IFAC-PapersOnLine. 50:11504-11508
Linear control theory has been long established and a myriad of techniques are available for designing controllers for linear systems in view of conflicting performance requirements. On the other hand, nonlinear control techniques are often tailored
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f3b9960fc2b80c5a6af40d6996d5f750
https://doi.org/10.1016/j.ifacol.2017.08.1609
https://doi.org/10.1016/j.ifacol.2017.08.1609
Publikováno v:
Journal of Guidance, Control, and Dynamics
Journal of Guidance, Control, and Dynamics, American Institute of Aeronautics and Astronautics, 2019, 42 (2), pp.303-316. ⟨10.2514/1.G003374⟩
Journal of Guidance, Control, and Dynamics, American Institute of Aeronautics and Astronautics, 2019, 42 (2), pp.303-316. ⟨10.2514/1.G003374⟩
International audience; This paper addresses fundamental issues in tail-sitting and transition flight aerodynamics modeling in view of sumof-squares (SOS) algorithmic guidance and control design. A novel approach, called ϕ theory, for modelingaerody
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::01e7fc1afbbcf989b1e2c5dd193c95ef
https://hal.archives-ouvertes.fr/hal-03035938
https://hal.archives-ouvertes.fr/hal-03035938
Autor:
Leandro R. Lustosa, Jacson M. O. Barth, Cédric Join, Michel Fliess, Murat Bronz, Jean-Philippe Condomines, Jean-Marc Moschetta
Publikováno v:
International Conference on Unmanned Aircraft Systems, ICUAS'18
International Conference on Unmanned Aircraft Systems, ICUAS'18, Jun 2018, Dallas, TX, United States. pp.1157-1164
HAL
International Conference on Unmanned Aircraft Systems, ICUAS'18, Jun 2018, Dallas, TX, United States. pp.1157-1164
HAL
International audience; Transitioning vehicles experience three different flight phases during typical missions. The hovering and forward flight phases have been researched widely, however the transition phase in between is more challenging and has b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::505c550ce03adf9cac04cba10865cbb2
https://hal-enac.archives-ouvertes.fr/hal-01817515
https://hal-enac.archives-ouvertes.fr/hal-01817515
Publikováno v:
Proceedings of the 2018 European Control Conference (ECC)
2018 European Control Conference (ECC)
2018 European Control Conference (ECC), Jun 2018, Limassol, Cyprus. pp.3120-3125, ⟨10.23919/ECC.2018.8550415⟩
ECC
2018 European Control Conference (ECC)
2018 European Control Conference (ECC), Jun 2018, Limassol, Cyprus. pp.3120-3125, ⟨10.23919/ECC.2018.8550415⟩
ECC
International audience; Quaternion algebra is frequently employed for spacecraft attitude description due to its convenient numerical properties when compared to minimal formulations. In parallel, Linear Quadratic Control (LQR)-based attitude control
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::73532f18a5f6d6fb0d30c7e3455f1ae9
https://hal.archives-ouvertes.fr/hal-01994381/file/Lustosa_21706.pdf
https://hal.archives-ouvertes.fr/hal-01994381/file/Lustosa_21706.pdf
Publikováno v:
MED
This paper details the design of a nonlinear controller for the Roll&Fly mode of a wheeled tilt-body micro air vehicle (MAV), developed at ISAE-SUPAERO, called the MAVion. The Roll&Fly mode consists in flying while rolling on walls or onto the ground
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::72b52fa9b0fc7c488187d32421b28aa2
https://doi.org/10.1109/med.2016.7536033
https://doi.org/10.1109/med.2016.7536033
It is well known that stand-alone inertial navigation systems (INS) have their errors diverging with time. Consequently an upper bound on the duration of INS systems precludes their use in low-cost micro unmanned aerial vehicles. The traditional appr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8a31db9f27cb07449c071d3f013d09c6
https://oatao.univ-toulouse.fr/16809/
https://oatao.univ-toulouse.fr/16809/
Publikováno v:
2015 International Conference on Unmanned Aircraft Systems (ICUAS).
This work studies a longitudinal high incidence flight envelope dynamic model for use in a convertible tilt-body vehicle designed for indoor/outdoor environments. The model assumptions are chosen so that a singularity-free nonlinear differential equa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::95fca59d77fa5a8ac8cc7012e3e14e9b
https://doi.org/10.1109/icuas.2015.7152366
https://doi.org/10.1109/icuas.2015.7152366
Autor:
Jacques Waldmann, Leandro R. Lustosa
Publikováno v:
Advances in Estimation, Navigation, and Spacecraft Control ISBN: 9783662447840
It is well-known that stand-alone inertial navigation systems (INS) have their errors diverging with time. The traditional approach for solving such incovenience is to resort to position and velocity aiding such as global navigation satellite systems
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::457f0cf70f9a6927a2fcb849b7b142e4
https://doi.org/10.1007/978-3-662-44785-7_15
https://doi.org/10.1007/978-3-662-44785-7_15
Publikováno v:
2015 International Conference on Unmanned Aircraft Systems (ICUAS); 2015, p816-824, 9p