ASTRADORS: Astrodynamics and Advanced Orbital Systems
The research group ASTRADORS was founded in April 2022 by Dr. Marcello Romano, when he joined POLITO/DIMEAS, as a Full Professor, via direct call.
The research interests and activities of the ASTRADORS research group are based upon, and further expand the activities of the Spacecraft Robotics Laboratory, which Prof. Marcello Romano founded in 2004, and directed thereafter, at the Naval Postgraduate School of Monterey, California.
In particular, the interests and activities of the research group ASTRADORS include:
- Classical Mechanics, Astrodynamics, and Astronautics: as it concerns the development, and analytical and numerical solution of mathematical models of both rotational and orbital flight, for application such as agile spacecraft attitude maneuvers, proximity maneuvers, and orbital maneuvers for space logistics and assembly of very large space systems.
- Autonomous spacecraft Guidance, Navigation & Control: as it concerns the design, implementation and experimental testing of real-time-capable algorithms. The algorithms are based on classical and optimal control theory, as well as on modern techniques, including AI/Machine Learning.
- Orbital Robotics: as it concerns the development of mathematical models for multi-body orbiting systems, for applications such as On-orbit Servicing, Assembly and Manufacturing, and Space Debris Removal.
- Space Systems Engineering & Technology Transfer: as it concerns the invention, modeling, simulation, design, and testing of advanced space systems and subsystems. Of particular interest are Satellite-Manipulator Systems, Tethered Satellite Systems, Distributed Space Systems and Self-assembled Very Large Space Systems.
- Space-based,system-of-systems for broad societal benefit: as it concerns, the conceptualization, mathematical modeling, and analysis of Space-Based Climate Change Mitigation Strategies (such as the Planetary Sunshade) and Space-Based Solar Power Systems.
The research methods utilized by the ASTRADORS research group include: analysis, numerical simulations, conceptualization and design, and experimental testing, both in the lab and on experimental space flights. In particular, as regards the lab experimental activity, a hardware-in-the-loop spaceflight emulator kino-dynamic test-bed is currently under development in the ASTRADORS lab at POLITO. The testbed will be functionally equivalent to the POSEYDIN test-bed previously developed by Prof. Marcello Romano at the Naval Postgraduate School, and shown in the picture.
Projects
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Selected funded research projects
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OPERAZIONI DI PROSSIMITÀ MULTISATELLITE PER MISSIONI DI RENDEZVOUS E DOCKING IN ORBITE TERRESTRI E LUNARI
ROMANO MARCELLO
2023 - 2025 (Current) -
ADVANCED SPACE TETHERS FOR REMOTE-SENSING OPERATIONS
ROMANO MARCELLO
2023 - 2025 (Current) -
ADVANCED SPACE TETHERS FOR REMOTE-SENSING APPLICATIONS
ROMANO MARCELLO
2024 - 2024 (Current) -
GRAVITY REDUCED APPROACH FOR VERSATILE AND INTEGRATED TESTING OF ARTIFICIAL SATELLITE PROXIMITY-MANEUVER SCENARIOS.
ROMANO MARCELLO
2023 - 2023 (Current) -
ATTIVITÀ DI RICERCA E SVILUPPO TECNOLOGICO CONCERNENTE IL DESIGN, LO SVILUPPO E LA QUALIFICA DELLA MISSIONE DIMOSTRATIVA DI IN-ORBIT SERVICING
ROMANO MARCELLO
2024 - 2024 (Completed)
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OPERAZIONI DI PROSSIMITÀ MULTISATELLITE PER MISSIONI DI RENDEZVOUS E DOCKING IN ORBITE TERRESTRI E LUNARI
Publications
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Selected recent publications
2024
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A distributed space radar sounder using a cross-track flying tethered satellite system
Article
Aliberti, Stefano; Quadrelli, Marco B.; Romano, Marcello
ACTA ASTRONAUTICA
Elsevier
Vol.221 pp.17 (pp.266-282) ISSN:0094-5765 DOI:10.1016/j.actaastro.2024.05.018
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Dynamics and Aerodynamic Control of a Cross-Track Tether Satellite System
Proceeding
Aliberti, Stefano; Quadrelli, B. Marco; Romano, Marcello
In: Titolo volume non avvalorato
ESA
ESA GNC-ICATT 2023 (Sopot, Poland) 12-16/06/2023
pp.15 DOI:10.5270/esa-gnc-icatt-2023-098 -
Development of a tip-tilt air-bearing testbed for physically emulating proximity-flight orbital mechanics
Article
Fernandez, B. R.; Herrera, L.; Hudson, J.; Romano, M.
ADVANCES IN SPACE RESEARCH
Elsevier
pp.8 ISSN:0273-1177 DOI:10.1016/j.asr.2023.01.005 -
Orbital hopping maneuvers with Astrobee on-board the International Space Station
Article
Kwok-Choon, Stephen T.; Romano, Marcello; Hudson, Jennifer
ACTA ASTRONAUTICA
Elsevier
Vol.207 pp.15 (pp.62-76) ISSN:0094-5765 DOI:10.1016/j.actaastro.2023.02.034
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On-orbit Demonstration of Spacecraft Hopping Maneuvers using the NASA Astrobee Free-Flyers
Proceeding
Hudson, Jennifer; Kwock-Choon, Stephen T.; Romano, Marcello
In: Proceedings
International Astronautical Federation
73rd International Astronautical Congress
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Orbital hopping maneuvers with two Astrobee free-flyers: Ground and flight experiments
Article
Kwok-Choon, Stephen; Hudson, Jennifer; Romano, Marcello
FRONTIERS IN ROBOTICS AND AI
FRONTIERS MEDIA SA
Vol.9 pp.14 ISSN:2296-9144 DOI:10.3389/frobt.2022.1004165
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Space Robotics
Book chapter
Romano, Marcello
Encyclopedia of Systems and Control
Springer
pp.8 (pp.2090-2097) ISBN:9783030441838 DOI:10.1007/978-3-030-44184-5_100035 -
Development and Experimentation of a CubeSat Magnetic Attitude Control System Testbed
Article
Cervettini, G.; Pastorelli, S.; Park, H.; Lee, D. Y.; Romano, M.
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS
Institute of Electrical and Electronics Engineers Inc.
Vol.57 pp.6 (pp.1345-1350) ISSN:0018-9251 DOI:10.1109/TAES.2020.3040032
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Angularly Unbounded Three-Axis Spacecraft Simulator
Patent
Chesi, Simone; Romano, Marcello
N.US 10,621,883 B2 -
An updated re-entry analysis of the Hubble Space Telescope
Article
Baker, Kyle; Culton, Eryn; Lang, Jonathan; Lewis, Zachary; Perez-Alemany, Robert; Rizzo, Alexa; Smeresky, Brendon; Starks, Anthony; Teneyck, Joshua; Rhatigan, Jennifer; Romano, Marcello
JOURNAL OF SPACE SAFETY ENGINEERING
Elsevier
Vol.7 pp.7 (pp.404-410) ISSN:2468-8967 DOI:10.1016/j.jsse.2020.07.006 -
Time-optimal control of linear time invariant systems between two arbitrary states
Article
Romano, Marcello; Curti, Fabio
AUTOMATICA
Elsevier
Vol.120 pp.9 ISSN:0005-1098 DOI:10.1016/j.automatica.2020.109151
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A convex-programming-based guidance algorithm to capture a tumbling object on orbit using a spacecraft equipped with a robotic manipulator
Article
Virgili-Llop, J.; Zagaris, C.; Zappulla, R.; Bradstreet, A.; Romano, M.
THE INTERNATIONAL JOURNAL OF ROBOTICS RESEARCH
SAGE Publications Inc.
Vol.38 pp.33 (pp.40-72) ISSN:0278-3649 DOI:10.1177/0278364918804660 -
Attitude stabilization of spacecraft in very low earth orbit by center-of-mass shifting
Article
Virgili-Llop, J.; Polat, H. C.; Romano, M.
FRONTIERS IN ROBOTICS AND AI
Frontiers Media S.A.
Vol.6 pp.19 ISSN:2296-9144 DOI:10.3389/frobt.2019.00007 -
Simultaneous capture and detumble of a resident space object by a free-flying spacecraft-manipulator system
Article
Virgili-Llop, J.; Romano, M.
FRONTIERS IN ROBOTICS AND AI
Frontiers Media S.A.
Vol.6 pp.24 ISSN:2296-9144 DOI:10.3389/frobt.2019.00014 -
Equilibrium-Based Force and Torque Control for an Aerial Manipulator to Interact with a Vertical Surface
Article
Tavora, B.; Park, H.; Romano, M.; Yun, X.
ROBOTICA
Cambridge University Press
Vol.38 pp.23 (pp.582-604) ISSN:0263-5747 DOI:10.1017/S0263574719000870 -
Real-Time Autonomous Spacecraft Proximity Maneuvers and Docking Using an Adaptive Artificial Potential Field Approach
Article
Zappulla, R.; Park, H.; Virgili-Llop, J.; Romano, M.
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
Institute of Electrical and Electronics Engineers Inc.
Vol.27 pp.8 (pp.2598-2605) ISSN:1063-6536 DOI:10.1109/TCST.2018.2866963 -
Historical survey of kinematic and dynamic spacecraft simulators for laboratory experimentation of on-orbit proximity maneuvers
Article
Wilde, M.; Clark, C.; Romano, M.
PROGRESS IN AEROSPACE SCIENCES
Elsevier Ltd
Vol.110 pp.26 ISSN:0376-0421 DOI:10.1016/j.paerosci.2019.100552 -
An Offline-Sampling SMPC Framework with Application to Autonomous Space Maneuvers
Article
Mammarella, Martina; Matthias, Lorenzen; Capello, Elisa; Hyeongjun, Park; Dabbene, Fabrizio; Guglieri, Giorgio; Romano, Marcello; Frank, Allgower
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
IEEE
pp.15 (pp.1-15) ISSN:1063-6536 DOI:10.1109/TCST.2018.2879938
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Experimental evaluation of model predictive control and inverse dynamics control for spacecraft proximity and docking maneuvers
Article
Virgili-Llop, J.; Zagaris, C.; Park, H.; Zappulla, R.; Romano, M.
CEAS SPACE JOURNAL
Springer-Verlag Wien
Vol.10 pp.13 (pp.37-49) ISSN:1868-2502 DOI:10.1007/s12567-017-0155-7 -
Reachability Analysis of Planar Spacecraft Docking with Rotating Body in Close Proximity
Article
Zagaris, Costantinos; Romano, Marcello
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.41 pp.7 (pp.1416-1422) ISSN:0731-5090 DOI:10.2514/1.G003389 -
Equations of Motion of Free-Floating Spacecraft-Manipulator Systems: An Engineer's Tutorial
Article
Wilde, Markus; Kwok Choon, Stephen; Grompone, Alessio; Romano, Marcello
FRONTIERS IN ROBOTICS AND AI
Frontiers
Vol.5 pp.24 ISSN:2296-9144 DOI:10.3389/frobt.2018.00041 -
Development and experimental validation of a multi-algorithmic hybrid attitude determination and control system for a small satellite
Article
Lee, Dae Young; Park, Hyeongjun; Romano, Marcello; Cutler, James
AEROSPACE SCIENCE AND TECHNOLOGY
Elsevier
Vol.78 pp.16 (pp.494-509) ISSN:1270-9638 DOI:10.1016/j.ast.2018.04.040 -
Model Predictive Control of Spacecraft Relative Motion with Convexified Keep-Out-Zone Constraints
Article
Zagaris, Costantinos; Park, Hyeongjun; Virgili-Llop, Josep; Zappulla, Richard; Romano, Marcello; Kolmanovsky, Ilya
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
American Institute of Aeronautics and Astronautics
Vol.41 pp.9 (pp.2054-2062) ISSN:0731-5090 DOI:10.2514/1.G003549 -
Artificial Potential Field and Sliding Mode Strategies for Proximity Operations with Obstacle Avoidance
Proceeding
Bloise, N.; Capello, E.; Park, H.; Punta, E.; Romano, M.
In: Proceedings of IEEE International Workshop on Variable Structure Systems
IEEE Computer Society
15th International Workshop on Variable Structure Systems, VSS 2018 (Graz University of Technology, aut) 2018
Vol.2018- pp.6 (pp.221-226) ISBN:9781538664391 DOI:10.1109/VSS.2018.8460264 -
Attitude Control of a Small Spacecraft for Earth Observation via Tube-based Robust Model Predictive Control
Proceeding
Mammarella, Martina; Young Lee, Dae; Park, Hyeongjun; Capello, Elisa; Dentis, Matteo; Guglieri, Giorgio; Romano, Marcello
In: AIAA SPACE 2018
AIAA (STATI UNITI D'AMERICA)
AIAA Space and Astronautics Forum and Exploration 2018 (Orlando, Florida) 17-19/09/2018
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Tube-based robust model predictive control for spacecraft proximity operations in the presence of persistent disturbance
Article
Mammarella, M.; Capello, E.; Park, H.; Guglieri, G.; Romano, M.
AEROSPACE SCIENCE AND TECHNOLOGY
Elsevier
Vol.77 pp.10 (pp.585-594) ISSN:1270-9638 DOI:10.1016/j.ast.2018.04.009
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Fast and Near-Optimal Guidance for Docking to Uncontrolled Spacecraft
Article
Ventura, Jacopo; Ciarcià, Marco; Romano, Marcello; Walter, Ulrich
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.40 pp.17 (pp.3138-3154) ISSN:0731-5090 DOI:10.2514/1.G001843 -
Dynamic Air-Bearing Hardware-in-the-Loop Testbed to Experimentally Evaluate Autonomous Spacecraft Proximity Maneuvers
Article
Zappulla, Richard; Virgili-Llop, Josep; Zagaris, Costantinos; Park, Hyeongjun; Romano, Marcello
JOURNAL OF SPACECRAFT AND ROCKETS
AIAA
Vol.54 pp.15 (pp.825-839) ISSN:0022-4650 DOI:10.2514/1.A33769 -
Aerodynamic Three-Axis Attitude Stabilization of a Spacecraft by Center-of-Mass Shifting
Article
Chesi, Simone; Gong, Qi; Romano, Marcello
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.40 pp.14 (pp.1613-1626) ISSN:0731-5090 DOI:10.2514/1.G002460 -
Emulating Scaled Clohessy–Wiltshire Dynamics on an Air-Bearing Spacecraft Simulation Testbed
Article
Ciarcià, Marco; Cristi, Roberto; Romano, Marcello
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.40 pp.15 (pp.2496-2510) ISSN:0731-5090 DOI:10.2514/1.G002585 -
Laboratory experiments of resident space object capture by a spacecraft–manipulator system
Article
Virgili-Llop, J.; Drew, J. V.; Zappulla, R.; Romano, M.
AEROSPACE SCIENCE AND TECHNOLOGY
Elsevier Masson SAS
Vol.71 pp.16 (pp.530-545) ISSN:1270-9638 DOI:10.1016/j.ast.2017.09.043 -
Spacecraft Thruster Control via Sigma–Delta Modulation
Article
Zappulla, Richard; Virgili-Llop, Josep; Romano, Marcello
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.40 pp.6 (pp.2928-2933) ISSN:0731-5090 DOI:10.2514/1.G002986 -
Spacecraft Proximity Operations Via Tube-Based Robust Model Predictive Control with Additive Disturbances
Proceeding
Mammarella, Martina; Capello, Elisa; Park, H.; Guglieri, Giorgio; Romano, M.
In: 68th International Astronautical Congress
International Astronautical Federation
68th International Astronautical Congress (Adelaide, Australia) September 25-29, 2017
Vol.1 pp.13 (pp.1-13)
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Experimental Characterization of Inverse Dynamics Guidance in Docking with a Rotating Target
Article
Wilde, Markus; Ciarcià, Marco; Grompone, Alessio; Romano, Marcello
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.39 pp.15 (pp.1173-1187) ISSN:0731-5090 DOI:10.2514/1.G001631 -
Survey, Statistical Analysis and Classification of Launched CubeSat Missions with Emphasis on the Attitude Control Method
Article
Polat, H. C.; Virgili-Llop, J.; Romano, Marcello
JOURNAL OF SMALL SATELLITES
Deepak Publishing
Vol.5 pp.18 (pp.513-530) ISSN:2327-4123
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Performance evaluation of the inverse dynamics method for optimal spacecraft reorientation
Article
Ventura, Jacopo; Romano, Marcello; Walter, Ulrich
ACTA ASTRONAUTICA
Elsevier
Vol.110 pp.13 (pp.266-278) ISSN:0094-5765 DOI:10.1016/j.actaastro.2014.11.041 -
Modeling and Experimental Parameter Identification of a Multicopter via a Compound Pendulum Test Rig
Proceeding
Capello, Elisa; Park, Hyeongjun; Tavora, Bruno; Guglieri, Giorgio; Romano, Marcello
In: 3rd RED-UAS 2015 - Workshop on Research, Education and Development of Unmanned Aerial Systems
3rd RED-UAS 2015 - Workshop on Research, Education and Development of Unmanned Aerial Systems (Cancun, Mexico) November 23-25, 2015
pp.10 (pp.1-10)
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A near-optimal guidance for cooperative docking maneuvers
Article
Ciarcià, Marco; Grompone, Alessio; Romano, Marcello
ACTA ASTRONAUTICA
Elsevier
Vol.102 pp.11 (pp.367-377) ISSN:0094-5765 DOI:10.1016/j.actaastro.2014.01.002 -
Characterization of a shape memory alloy interference coupling
Article
Crane, W. M.; Newman, J. H.; Romano, M.
SMART MATERIALS AND STRUCTURES
Institute of Physics Publishing
Vol.23 pp.6 ISSN:0964-1726 DOI:10.1088/0964-1726/23/11/115011 -
Exact analytic solution for the spin-up maneuver of an axially symmetric spacecraft
Article
Ventura, Jacopo; Romano, Marcello
ACTA ASTRONAUTICA
Elsevier
Vol.104 pp.17 (pp.324-340) ISSN:0094-5765 DOI:10.1016/j.actaastro.2014.07.038
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Simulations of Multiple Spacecraft Maneuvering with MATLAB/Simulink and Satellite Tool Kit
Article
Mccamish, Shawn B.; Ciarcià, Marco; Romano, Marcello
JOURNAL OF AEROSPACE INFORMATION SYSTEMS
AIAA
Vol.10 pp.11 (pp.348-358) ISSN:2327-3097 DOI:10.2514/1.35328
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Development and experimentation of LQR/APF guidance and control for autonomous proximity maneuvers of multiple spacecraft
Article
Bevilacqua, R.; Lehmann, T.; Romano, M.
ACTA ASTRONAUTICA
Elsevier
Vol.68 pp.16 (pp.1260-1275) ISSN:0094-5765 DOI:10.1016/j.actaastro.2010.08.012 -
Time-Optimal Reorientation of a Spacecraft Using an Inverse Dynamics Optimization Method
Article
Boyarko, George A.; Romano, Marcello; Yakimenko, Oleg A.
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AiAA
Vol.34 pp.12 (pp.1197-1208) ISSN:0731-5090 DOI:10.2514/1.49449 -
Optimal Rendezvous Trajectories of a Controlled Spacecraft and a Tumbling Object
Article
Boyarko, George; Yakimenko, Oleg; Romano, Marcello
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.34 pp.14 (pp.1239-1252) ISSN:0731-5090 DOI:10.2514/1.47645
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Multiple spacecraft rendezvous maneuvers by differential drag and low thrust engines
Article
Bevilacqua, R.; Hall, J. S.; Romano, M.
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY
Springer Netherlands
Vol.106 pp.20 (pp.69-88) ISSN:0923-2958 DOI:10.1007/s10569-009-9240-3 -
Decoupled-natural-dynamics model for the relative motion of two spacecraft without and with J2 perturbation
Article
Bevilacqua, R.; Romano, M.; Curti, F.
NONLINEAR DYNAMICS AND SYSTEMS THEORY
Kiev: Informath Publishing Group.
Vol.10 pp.10 (pp.11-20) ISSN:1562-8353 -
Autonomous distributed control of simultaneous multiple spacecraft proximity maneuvers
Article
Mccamish, S. B.; Romano, M.; Yun, X.
IEEE TRANSACTIONS ON AUTOMATION SCIENCE AND ENGINEERING
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
Vol.7 pp.15 (pp.630-644) ISSN:1545-5955 DOI:10.1109/TASE.2009.2039010 -
Detumbling and nutation canceling maneuvers with complete analytic reduction for axially symmetric spacecraft
Article
Romano, Marcello
ACTA ASTRONAUTICA
Elsevier
Vol.66 pp.10 (pp.989-998) ISSN:0094-5765 DOI:10.1016/j.actaastro.2009.09.015 -
Lyapunov-Based Thrusters' Selection for Spacecraft Control: Analysis and Experimentation
Article
Curti, Fabio; Romano, Marcello; Bevilacqua, Riccardo
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.33 pp.18 (pp.1143-1160) ISSN:0731-5090 DOI:10.2514/1.47296
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Online generation of quasi-optimal spacecraft rendezvous trajectories
Article
Bevilacqua, R.; Romano, M.; Yakimenko, O.
ACTA ASTRONAUTICA
Pergamon Press
Vol.64 pp.14 (pp.345-358) ISSN:0094-5765 DOI:10.1016/j.actaastro.2008.08.001 -
A ballistic-pendulum test stand to characterize small cold-gas thruster nozzles
Article
Lugini, Claudio; Romano, Marcello
ACTA ASTRONAUTICA
Pergamon Press
Vol.64 pp.11 (pp.615-625) ISSN:0094-5765 DOI:10.1016/j.actaastro.2008.11.001 -
Ad Hoc Wireless Networking and Shared Computation for Autonomous Multirobot Systems
Article
Bevilacqua, Riccardo; Hall, Jason S.; Horning, James; Romano, Marcello
JOURNAL OF AEROSPACE COMPUTING, INFORMATION, AND COMMUNICATION
AiAA
Vol.6 pp.26 (pp.328-353) ISSN:1542-9423 DOI:10.2514/1.40734 -
Flight Testing of Multiple-Spacecraft Control on SPHERES During Close-Proximity Operations
Article
Mccamish, Shawn B.; Romano, Marcello; Nolet, Simon; Edwards, Christine M.; Miller, David W.
JOURNAL OF SPACECRAFT AND ROCKETS
AIAA
Vol.46 pp.12 (pp.1202-1213) ISSN:0022-4650 DOI:10.2514/1.43563
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Exact analytic solution for the rotation of a rigid body having spherical ellipsoid of inertia and subjected to a constant torque
Article
Romano, Marcello
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY
SPRINGER
Vol.100 pp.9 (pp.181-189) ISSN:0923-2958 DOI:10.1007/s10569-007-9112-7 -
Exact analytic solutions for the rotation of an axially symmetric rigid body subjected to a constant torque
Article
Romano, Marcello
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY
SPRINGER
Vol.101 pp.16 (pp.375-390) ISSN:0923-2958 DOI:10.1007/s10569-008-9155-4 -
Rendezvous Maneuvers of Multiple Spacecraft Using Differential Drag Under J2 Perturbation
Article
Bevilacqua, R.; Romano, M.
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.31 pp.13 (pp.1595-1607) ISSN:0731-5090 DOI:10.2514/1.36362 -
Rendezvous maneuvers of multiple spacecraft using differential drag under J2 perturbation
Proceeding
Bevilacqua, R.; Romano, M.
In: AIAA Guidance, Navigation and Control Conference and Exhibit
American Institute of Aeronautics and Astronautics Inc.
AIAA Guidance, Navigation and Control Conference and Exhibit
DOI:10.2514/6.2008-6828
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Laboratory Experimentation of Autonomous Spacecraft Approach and Docking to a Collaborative Target
Article
Romano, Marcello; Friedman, David A.; Shay, Tracy J.
JOURNAL OF SPACECRAFT AND ROCKETS
AIAA
Vol.44 pp.10 (pp.164-173) ISSN:0022-4650 DOI:10.2514/1.22092 -
Fuel-Optimal Spacecraft Rendezvous with Hybrid On-Off Continuous and Impulsive Thrust
Article
Bevilacqua, Riccardo; Romano, Marcello
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.30 pp.4 (pp.1175-1178) ISSN:0731-5090 DOI:10.2514/1.27716
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Attitude Dynamics/Control of a Dual-Body Spacecraft with Variable-Speed Control Moment Gyros
Article
Romano, Marcello; Agrawal, Brij N.
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.27 pp.13 (pp.513-525) ISSN:0731-5090 DOI:10.2514/1.2564
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Experiments on Command Shaping Control of a Manipulator with Flexible Links
Article
Romano, Marcello; Agrawal, Brij N.; Bernelli-Zazzera, Franco
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
AIAA
Vol.25 pp.8 (pp.232-239) ISSN:0731-5090 DOI:10.2514/2.4903
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A distributed space radar sounder using a cross-track flying tethered satellite system