Dieses Bild zeigtFabrizio Turco

Fabrizio Turco

Herr M.Sc.

Wissenschaftlicher Mitarbeiter
Institut für Raumfahrtsysteme
Raumtransporttechnologie

Kontakt

+49 711 685 62394

Pfaffenwaldring 29
70569 Stuttgart
Deutschland
Raum: 2.34

  1. 2026

    1. 1. F. Turco, C. Traub, and S. Fasoulas, “Uncertainty-Aware Aerodynamic Orbit Control in Very Low Earth Orbits,” in AAS/AIAA Astrodynamics Specialist Conference, Jul. 2026.
    2. 2. F. Turco, C. Traub, and S. Fasoulas, “Decay-optimal lift-based adjustments of the orbital plane in Very Low Earth Orbits,” Acta Astronautica, Sep. 2026, doi: 10.1016/j.actaastro.2026.04.025.
    3. 3. F. Turco, C. Traub, M. Schütte, M. Pfeiffer, and S. Fasoulas, “Assessment of the practicality of optimal aerodynamic orbit control in VLEO,” Acta Astronautica, Aug. 2026, doi: 10.1016/j.actaastro.2026.02.039.
    4. 4. C. Traub et al., “Preparation of a First Ever In-Orbit Demonstration of Differential Lift in INTA’s ANSER Cluster,” in International Symposium on Space Flight Dynamics, Toulouse, France, Jun. 2026.
    5. 5. J. Boskovic et al., “Uncertainty Is Certain: Sources, Modeling, and Impacts of Uncertainty for VLEO Satellites,” May 2026. [Online]. Available: https://www.researchgate.net/publication/403437176_Uncertainty_Is_Certain_Sources_Modeling_and_Impacts_of_Uncertainty_for_VLEO_Satellites

  2. 2025

    1. 6. F. E. G. Turco, C. Traub, and S. Fasoulas, “Optimal Satellite Orbit Control via Aerodynamic Forces in Very Low Earth Orbits,” in AAS/AIAA Astrodynamics Specialist Conference, Aug. 2025. [Online]. Available: https://www.researchgate.net/publication/394530650_Optimal_Satellite_Orbit_Control_via_Aerodynamic_Forces_in_Very_Low_Earth_Orbits
    2. 7. F. Turco, C. Traub, M. Schütte, M. Pfeiffer, and S. Fasoulas, “Assessment of the Practicality of Optimal Aerodynamic Orbit Control in VLEO,” in IAF Astrodynamics Symposium, Sep. 2025. doi: 10.52202/083087-0029.
    3. 8. C. Traub et al., “Revealing the impact of operational constraints on aerodynamic collision avoidance maneuvers : In-flight results from the BEESAT-4 CubeSat,” Acta astronautica, vol. 234, Art. no. September, 2025, doi: 10.1016/j.actaastro.2025.04.038.
    4. 9. L. Ingrillini et al., “Operationalizing differential drag control : a planning routine for the S-NET satellite formation,” CEAS space journal, 2025, doi: 10.1007/s12567-025-00630-x.
    5. 10. P. Haufe et al., “Minimum-Time Spacecraft Collision Avoidance Using Aerodynamic Lift and Drag Via Reachable Sets,” in 23rd IAA Symposium on Space Debris, Oct. 2025. doi: 10.52202/083079-0150.
    6. 11. E. Gaglio et al., “Quasi-Optimal Guidance and Control in Very Low Earth Orbit via Deep Learning for Drag-Based Collision Avoidance,” Acta astronautica, vol. 235, pp. 362–374, 2025, doi: 10.1016/j.actaastro.2025.05.029.
    7. 12. E. Gaglio, C. Traub, F. Turco, J. O. Murcia Piñeros, R. Bevilacqua, and S. Fasoulas, “Optimal drag-based collision avoidance: Balancing miss distance and orbital decay,” Acta Astronautica, vol. 228, pp. 295–305, Mar. 2025, doi: 10.1016/j.actaastro.2024.11.052.
    8. 13. S. Förste, L. E. Yousfi, J.-S. Fischer, F. Turco, C. Traub, and S. Fasoulas, “A comprehensive assessment of rocket body related space debris and discussion of suitable means of risk reduction,” Acta Astronautica, May 2025, doi: 10.1016/j.actaastro.2025.01.068.

  3. 2024

    1. 14. S. Zajonz et al., “Development of a Ferrofluid-Based Attitude Control Actuator for Verification on the ISS,” Aerotecnica Missili & Spazio, vol. 103, Art. no. 3, Sep. 2024, doi: 10.1007/s42496-024-00208-6.
    2. 15. F. Turco, C. Traub, S. Gaißer, J. C. Burgdorf, S. Klinkner, and S. Fasoulas, “Analysis of Collision Avoidance Manoeuvres Using Aerodynamic Drag for the Flying Laptop Satellite,” Aerotecnica missili & spazio, vol. 103, pp. 61–71, 2024, doi: 10.1007/s42496-023-00183-4.
    3. 16. S. Sütterlin et al., “Fargo : validation of space-relevant ferrofluid applications on the ISS,” CEAS space journal, vol. 16, Art. no. 6, 2024, doi: 10.1007/s12567-024-00539-x.
    4. 17. B. Karahan et al., “Recent results of Ferrofluid ISS Experiments to enable Sustainable Space Activities,” Journal of evolving space activities, vol. 2, p. 157, 2024, doi: 10.57350/jesa.157.
    5. 18. B. Karahan et al., “In-orbit validation of a ferrofluidic Thermal Switch in ISS microgravity,” CEAS space journal, 2024, doi: 10.1007/s12567-024-00579-3.
    6. 19. E. Gaglio, C. Traub, F. E. G. Turco, J. O. Murcia-Piñeros, R. Bevilacqua, and S. Fasoulas, “Optimal spacecraft collision avoidance using aerodynamic drag,” in 4th IAA Conference on Space Situational Awareness (ICSSA), May 2024.

  4. 2023

    1. 20. F. Turco, C. Traub, and S. Fasoulas, “Effects of solar and geomagnetic activity on aerodynamic collision avoidance manoeuvres.” Unpublished, 2023. doi: 10.13140/RG.2.2.17321.57442.
    2. 21. F. Turco, C. Traub, S. Gaißer, J. Burgdorf, S. Klinkner, and S. Fasoulas, “An analysis tool for collision avoidance manoeuvres using aerodynamic drag,” Acta astronautica, vol. 211, Art. no. October, 2023, doi: 10.1016/j.actaastro.2023.05.038.

  5. 2022

    1. 22. F. Turco, “Design and Implementation of a Tool to Simulate Collision Avoidance Using Aerodynamic Drag for the Flying Laptop,” Master Thesis, Unversity of Stuttgart, Stuttgart, Germany, 2022.

  6. 2019

    1. 23. F. Turco, “Experimentelle und analytische Untersuchung von Skalierungseffekten gepulster Plasmatriebwerke am Beispiel PETRUS 17J,” Bachelor Thesis, University of Stuttgart, Stuttgart, Germany, 2019.
Zum Seitenanfang