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Urbano Tancredi
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Citata da
Anno
Great circle navigation with vectorial methods
V Nastro, U Tancredi
The Journal of navigation 63 (3), 557-563, 2010
372010
Active debris multi-removal mission concept based on hybrid propulsion
P Tadini, U Tancredi, M Grassi, L Anselmo, C Pardini, A Francesconi, ...
Acta Astronautica 103, 26-35, 2014
362014
Ionospheric path delay models for spaceborne GPS receivers flying in formation with large baselines
U Tancredi, A Renga, M Grassi
Advances in Space Research 48 (3), 507-520, 2011
332011
Relative navigation in LEO by carrier-phase differential GPS with intersatellite ranging augmentation
A Renga, M Grassi, U Tancredi
International Journal of Aerospace Engineering 2013, 2013
302013
Real-time hardware-in-the-loop tests of star tracker algorithms
G Rufino, D Accardo, M Grassi, G Fasano, A Renga, U Tancredi
International Journal of Aerospace Engineering 2013, 2013
272013
Fast vertical trajectory prediction method for air traffic management, and relevant atm system
D Accardo, A Moccia, M Grassi, U Tancredi, L Caminiti, L Fiorillo, A Leardi, ...
US Patent 9,031,720, 2015
252015
Active removal of large massive objects by hybrid propulsion module
LT DeLuca, M Lavagna, F Maggi, P Tadini, C Pardini, L Anselmo, ...
5th European Conference for Aeronautics and Space Sciences (EUCASS), Munich …, 2013
182013
Relative positioning of spacecraft in intense ionospheric conditions by GPS
U Tancredi, G Allende-Alba, A Renga, O Montenbruck, M Grassi
Aerospace Science and Technology 43, 191-198, 2015
162015
Real-time relative positioning of spacecraft over long baselines
U Tancredi, A Renga, M Grassi
Journal of Guidance, Control, and Dynamics 37 (1), 47-58, 2014
162014
An algorithm for managing aircraft movement on an airport surface
U Tancredi, D Accardo, G Fasano, A Renga, G Rufino, G Maresca
Algorithms 6 (3), 494-511, 2013
162013
Validation on flight data of a closed-loop approach for GPS-based relative navigation of LEO satellites
U Tancredi, A Renga, M Grassi
Acta Astronautica 86, 126-135, 2013
142013
GPS-based relative navigation of LEO formations with varying baselines
U Tancredi, A Renga, M Grassi
AIAA Guidance, Navigation, and Control Conference, 8189, 2010
132010
Accurate ionospheric delay model for real-time GPS-based positioning of LEO satellites using horizontal VTEC gradient estimation
A Renga, F Causa, U Tancredi, M Grassi
Gps Solutions 22, 1-14, 2018
112018
Large debris removal mission in LEO based on hybrid propulsion
LT DeLuca, M Lavagna, F Maggi, P Tadini, C Pardini, L Anselmo, ...
Aerotecnica Missili & Spazio 93, 51-58, 2014
102014
Carrier-based Differential GPS for autonomous relative navigation in LEO
U Tancredi, A Renga, M Grassi
AIAA Guidance, Navigation, and Control Conference, 4707, 2012
102012
A novel method for flight control laws robustness analysis over unsteady trajectories
U Tancredi, M Grassi, F Corraro, E Filippone, R Palumbo, M Russo
IFAC Proceedings Volumes 40 (7), 347-352, 2007
92007
Novel closed-loop approaches for precise relative navigation of widely separated GPS receivers in LEO
U Tancredi, A Renga, M Grassi
Acta Astronautica 93, 243-251, 2014
82014
Navigation facility for high accuracy offline trajectory and attitude estimation in airborne applications
A Renga, G Fasano, D Accardo, M Grassi, U Tancredi, G Rufino, ...
International Journal of Navigation and Observation 2013, 2013
82013
Robustness analysis for terminal phases of reentry flight
U Tancredi, M Grassi, F Corraro, E Filippone
Journal of guidance, control, and dynamics 32 (5), 1679-1683, 2009
82009
Aerodynamics uncertainties compliance with desired lateral-directional dynamics for an unmanned space vehicle
U Tancredi, M Grassi, L Verde, F Corraro
Infotech@ Aerospace, 6962, 2005
72005
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
Articoli 1–20