Gianmarco Radice
Gianmarco Radice
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Backstepping control design with actuator torque bound for spacecraft attitude maneuver
I Ali, G Radice, J Kim
Journal of guidance, control, and dynamics 33 (1), 254-259, 2010
Quaternion-based finite time control for spacecraft attitude tracking
S Wu, G Radice, Y Gao, Z Sun
Acta Astronautica 69 (1-2), 48-58, 2011
Multicriteria comparison among several mitigation strategies for dangerous near-earth objects
JP Sanchez, C Colombo, M Vasile, G Radice
Journal of Guidance, Control, and Dynamics 32 (1), 121-142, 2009
Advanced global optimisation for mission analysis and design
DR Myatt, VM Becerra, SJ Nasuto, JM Bishop, D Izzo
Final Report. Ariadna id 3, 4101, 2004
Semi-analytical solution for the optimal low-thrust deflection of near-earth objects
C Colombo, M Vasile, G Radice
Journal of Guidance, Control, and Dynamics 32 (3), 796-809, 2009
Optimal low-thrust trajectories to asteroids through an algorithm based on differential dynamic programming
C Colombo, M Vasile, G Radice
Celestial mechanics and dynamical astronomy 105, 75-112, 2009
Close proximity formation flying via linear quadratic tracking controller and artificial potential function
L Palacios, M Ceriotti, G Radice
Advances in Space Research 56 (10), 2167-2176, 2015
Robust finite-time control for flexible spacecraft attitude maneuver
S Wu, G Radice, Z Sun
Journal of Aerospace Engineering 27 (1), 185-190, 2014
Comparison of single and multi‐spacecraft configurations for NEA deflection by solar sublimation
C Maddock, JP Sanchez Cuartielles, M Vasile, G Radice
AIP conference Proceedings 886 (1), 303-316, 2007
Potential approach for constrained autonomous manoeuvres of a spacecraft equipped with a cluster of control moment gyroscopes
G Avanzini, G Radice, I Ali
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2009
Preliminary space mission design under uncertainty
N Croisard, M Vasile, S Kemble, G Radice
Acta Astronautica 66 (5-6), 654-664, 2010
Robust attitude maneuver control of spacecraft with reaction wheel low-speed friction compensation
S Wu, R Wang, G Radice, Z Wu
Aerospace Science and Technology 43, 213-218, 2015
Robust optimal sun-pointing control of a large solar power satellite
S Wu, K Zhang, H Peng, Z Wu, G Radice
Acta Astronautica 127, 226-234, 2016
Locating large solar power satellites in the geosynchronous Laplace plane
I McNally, D Scheeres, G Radice
Journal of Guidance, Control, and Dynamics 38 (3), 489-505, 2015
Spiral trajectories in global optimisation of interplanetary and orbital transfers
M Vasile, O Schütze, O Junge, G Radice, M Dellnitz, D Izzo
Ariadna study report ao4919 5, 4106, 2006
Adaptive control for spacecraft relative translation with parametric uncertainty
S Wu, Z Wu, G Radice, R Wang
Aerospace Science and Technology 31 (1), 53-58, 2013
Multi-objective integrated robust H∞ control for attitude tracking of a flexible spacecraft
S Wu, W Chu, X Ma, G Radice, Z Wu
Acta Astronautica 151, 80-87, 2018
A Multi‐criteria assessment of deflection methods for dangerous NEOs
JP Sanchez Cuartielles, C Colombo, M Vasile, G Radice
AIP conference proceedings 886 (1), 317-336, 2007
Attitude dynamics of large geosynchronous solar power satellites
IJ McNally, DJ Scheeres, G Radice
AIAA/AAS Astrodynamics Specialist Conference, 4123, 2014
Ant colony algorithms for two impluse interplanetary trajectory optimization
G Radice, G Olmo
Journal of guidance, control, and dynamics 29 (6), 1440-1444, 2006
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