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  • CubETH: nano-satellite mission for orbit and attitude determination using low-cost GNSS receivers

    Paper number

    IAC-15,B4,4,5,x30129

    Author

    Dr. Anton Ivanov, Ecole Polytechnique Fédérale de Lausanne (EPFL), Space Engineering Center (eSpace), Switzerland

    Coauthor

    Mr. Stefano Rossi, Swiss Space Center, Switzerland

    Coauthor

    Mr. Nikolay Mullin, Bauman Moscow State Technical University, Russian Federation

    Coauthor

    Mr. Federico Belloni, Swiss Space Center, Switzerland

    Coauthor

    Mr. Reto Wiesendanger, Space Center EPFL, Switzerland

    Coauthor

    Mr. Louis Masson, Ecole Polytechnique Fédérale de Lausanne (EPFL), Swiss Space Center (SSC), Switzerland

    Coauthor

    Prof. Markus Rothacher, ETHZ Institute of Geodesy and Photogrammetry, Switzerland

    Coauthor

    Dr. Christine Hollenstein, ETHZ Institute of Geodesy and Photogrammetry, Switzerland

    Coauthor

    Mr. Benjamin Mannel, ETHZ Institute of Geodesy and Photogrammetry, Switzerland

    Coauthor

    Mr. Patrick Fleischmann, HSR University of Applied Sciences of Eastern Switzerland, Switzerland

    Coauthor

    Prof. Heinz Mathis, HSR University of Applied Sciences of Eastern Switzerland, Switzerland

    Coauthor

    Prof. Martin Klaper, Lucerne University of Applied Sciences and Arts (HSLU), Switzerland

    Coauthor

    Prof. Marcel Joss, Lucerne University of Applied Sciences and Arts (HSLU), Switzerland

    Coauthor

    Prof. Erich Styger, Lucerne University of Applied Sciences and Arts (HSLU), Switzerland

    Coauthor

    Mr. Daniel Willi, ETHZ Institute of Geodesy and Photogrammetry, Switzerland

    Year

    2015

    Abstract
    The CubETH satellite is a cooperative Swiss CubeSat mission involving Swiss Federal Universities (EPF Lausanne and ETH Zurich), Universities of Applied Sciences and Swiss companies. Тhe main objective of CubETH is to demonstrate new technologies in the area of GNSS-based navigation and use of COTS components. The satellite will carry five GNSS patch antennas, each connected to two independent u-blox multi-GNSS receivers. These very small, commercially available low-cost receivers are able to track single-frequency code and phase data of all the major GNSS, i.e. GPS, GLONASS, QZSS, Beidou (and ready for Galileo). This project makes intensive use of COTS technologies for microelectronics. To mitigate risk, we started the project with numerous tests to study the behavior of the receivers in the intended space environment and to evaluate their usability for space applications. 
    
    Four main science objectives have been defined for the CubETH mission: (1) precise orbit determination using low-cost GNSS receivers, (2) attitude determination based on very short baselines, (3) comparison of the performance in space between GPS and GLONASS (and possibly other GNSS) as an important step for further developments of space-borne GNSS receivers, (4) additional experimental measurements (e.g. for air density estimation during re-entry). The satellite will carry 3 retro-reflectors to enable satellite laser ranging for performance validation of the precise orbit determination. 
    
    Novel Cubesat technologies will also be tested. We will take into account lessons learned from the SwissCube mission, which is in operation since 2009. A new modular design for the structure as well as connectors will be flown. We also intend to demonstrate the use of a miniaturized low-power command and data handling system, which shall control the satellite. In this paper, we will present the reasons for new technologies, based on our experience with SwissCube. 
    
    Beyond these scientific and technological goals, CubETH will be a milestone for the Swiss space community. From the educational point of view, CubETH provides a valuable practical experience for students in space technologies, geodesy, computational and electrical sciences involved in the project. Participating institutions and industrial partners benefit from the joint development of seminal nano-satellite concepts and miniaturized components. This will be important concerning future formation flying and constellation missions, where miniaturized, inexpensive satellites and sensors are crucial. Overall, the space community in Switzerland will benefit from the CubETH mission by the acquisition of relevant expertise and technology for future small satellite missions.
    Abstract document

    IAC-15,B4,4,5,x30129.brief.pdf

    Manuscript document

    IAC-15,B4,4,5,x30129.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.