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Mirko Leomanni
Mirko Leomanni
Research Fellow, University of Perugia
Verified email at unipg.it
Title
Cited by
Cited by
Year
Explicit model predictive control approach for low-thrust spacecraft proximity operations
M Leomanni, E Rogers, SB Gabriel
Journal of Guidance, Control, and Dynamics 37 (6), 1780-1790, 2014
902014
Propulsion options for very low Earth orbit microsatellites
M Leomanni, A Garulli, A Giannitrapani, F Scortecci
Acta Astronautica 133, 444-454, 2017
802017
Autonomous low-Earth-orbit station-keeping with electric propulsion
A Garulli, A Giannitrapani, M Leomanni, F Scortecci
Journal of guidance, control, and dynamics 34 (6), 1683-1693, 2011
562011
Orbit control techniques for space debris removal missions using electric propulsion
M Leomanni, G Bianchini, A Garulli, A Giannitrapani, R Quartullo
Journal of Guidance, Control, and Dynamics 43 (7), 1259-1268, 2020
232020
An MPC-based attitude control system for all-electric spacecraft with on/off actuators
M Leomanni, A Garulli, A Giannitrapani, F Scortecci
52nd IEEE conference on decision and control, 4853-4858, 2013
212013
Spacecraft localization via angle measurements for autonomous navigation in deep space missions
N Ceccarelli, A Garulli, A Giannitrapani, M Leomanni, F Scortecci
IFAC Proceedings Volumes 40 (7), 551-556, 2007
17*2007
Sum-of-norms model predictive control for spacecraft maneuvering
M Leomanni, G Bianchini, A Garulli, A Giannitrapani, R Quartullo
IEEE Control Systems Letters 3 (3), 649-654, 2019
162019
All-electric spacecraft precision pointing using model predictive control
M Leomanni, A Garulli, A Giannitrapani, F Scortecci
Journal of Guidance, Control, and Dynamics 38 (1), 161-168, 2015
162015
A class of globally stabilizing feedback controllers for the orbital rendezvous problem
M Leomanni, G Bianchini, A Garulli, A Giannitrapani
International journal of robust and nonlinear control 27 (18), 4607-4621, 2017
132017
Optimal low-thrust orbit transfers made easy: A direct approach
M Leomanni, G Bianchini, A Garulli, R Quartullo, F Scortecci
Journal of Spacecraft and Rockets 58 (6), 1904-1914, 2021
122021
State feedback control in equinoctial variables for orbit phasing applications
M Leomanni, G Bianchini, A Garulli, A Giannitrapani
Journal of Guidance, Control, and Dynamics 41 (8), 1815-1822, 2018
122018
Minimum switching control for systems of coupled double integrators
A Garulli, A Giannitrapani, M Leomanni
Automatica 60, 115-121, 2015
122015
Comparison of control laws for magnetic detumbling
M Leomanni
University of Siena. Research Gate. https://www. researchgate. netá…, 2012
112012
Satellite relative motion modeling and estimation via nodal elements
M Leomanni, A Garulli, A Giannitrapani, R Quartullo
Journal of Guidance, Control, and Dynamics 43 (10), 1904-1914, 2020
102020
Minimum switching limit cycle oscillations for systems of coupled double integrators
A Garulli, A Giannitrapani, M Leomanni
53rd IEEE Conference on Decision and Control, 4655-4660, 2014
102014
Precise attitude control of all-electric GEO spacecraft using Xenon microthrusters
M Leomanni, A Garulli, A Giannitrapani, F Scortecci
33rd International Electric Propulsion Conference, 2013
102013
Minimum switching thruster control for spacecraft precision pointing
M Leomanni, A Garulli, A Giannitrapani, F Farina, F Scortecci
IEEE Transactions on Aerospace and Electronic Systems 53 (2), 683-697, 2017
92017
Attitude and orbit control techniques for spacecraft with electric propulsion
M Leomanni
Ph. D. Dissertation, Dept. of Information Engineering and Mathematics, Univá…, 2015
92015
Variable-Horizon Guidance for Autonomous Rendezvous and Docking to a Tumbling Target
M Leomanni, R Quartullo, G Bianchini, A Garulli, A Giannitrapani
Journal of Guidance, Control, and Dynamics, 2022
82022
The applicability of pulsed plasma thrusters to rendezvous and docking of cubesats
S Gabriel, E Rogers, M Leomanni
33rd International Electric Propulsion Conference, 2013
82013
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