Educational nanosatellite detumbling simulator

• Autorzy: Postulka B. , Rachucki J. , Moczała B. , Zagórski P. , Gallina A.
• Języki publikacji: EN

Abstrakty

EN

The paper presents an overview of the educational nanosatellite detumbling simulator used as an educational tool at AGH University of Science and Technology in Krakow. The simulator consists of a Helrnholtz cage and semi-spherical air bearing used with a highly configurable test article that represents the satellite performing the detumbling manoeuvre. All those elements are supplemented with their respective software tools, developed in-house. This facility is used as part of a student project, where small teams will design and implement an attitude control system for detumbling the spacecraft based on the b-dot algorithm. Theoretical and practical aspects are combined in the students' project for increasing learning effects.

Słowa kluczowe

EN

space robotics; simulator; nano-satellite

PL

robotyka kosmiczna; symulator; nanosatelita

• Wydawca: Oficyna Wydawnicza Politechniki Warszawskiej
• Czasopismo: Prace Naukowe Politechniki Warszawskiej. Elektronika
• Rocznik: 2018
• Tom: z. 196
• Strony: 97--104
• Opis fizyczny: Bibliogr. 6 poz., rys., wykr.

Twórcy

autor

Postulka B.

• Faculty of Mechanical Engineering and Robotics, AGH University of Science and Technology, Al. A. Mickiewicza 30, 30-059 Krakow, Poland

autor

Rachucki J.

• HYPERSKY Space Technologies

autor

Moczała B.

autor

Zagórski P.

• Faculty of Electrical, Engineering, Automatics Computer Science and Biomedical Engineering, AGH University of Science and Technology, Al. A. Mickiewicza 30, 30-059 Krakow, Poland

autor

Gallina A.

• Faculty of Mechanical Engineering and Robotics, AGH University of Science and Technology, Al. A. Mickiewicza 30, 30-059 Krakow, Poland

Bibliografia

• [1] S. Lee et. al. CubeSat Design Specification, Cal Poly SLO, 2015.
• [2] M. Swartwout, University-class satellites: from marginal utility to 'disruptive' research platforms. Proceedings of AIAA/USU Conference on Small Satellites (SSC04-II-5), AIAA/USU, Logan, UT, 2004.
• [3] P. Zagorski, P. Bangert, A. Gallina, Identification of the orbit semi-major axis using frequency properties of onboard magnetic field measurements. Aerospace Science and Technology, Vol. 66, pp. 380-391, 2017.
• [4] P. Zagorski, T. Dziwinski, A. Tutaj, Steepest descent quaternion attitude estimator. Aerospace Science and Technology, Vol. 77, pp. 1-10, 2018.
• [5] A. Gallina, P. Zagorski, J. Rachucki, Test bed for simulation of magnetic field measurements of low Earth orbit satellites. Mechanics and Control, Vol. 34, No. 3, pp. 47-51, 2015.
• [6] A. J. Zmuda, 1971. The International Geomagnetic Reference Field in World Magnetic Survey Ed. A. J. Zmuda, IAGA Bulletin, No. 28, IUGG, Paris, 1957-1969.

Uwagi

PL

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).