A distributed nanosatellite attitude testing laboratory for joint research activities
نویسندگان
چکیده
Abstract. During the last decades, there has been an increase in use of satellites reduced dimensions. Among others, microsatellites (mass from 11 to 200 kg) and nanosatellites (1 10 have ones receiving increasing interest Universities for educational activities [1], [2]. Their cost, complexity developing time compared larger make them particularly suitable student projects. In this regard CubeSats (satellites standardised dimensions, based on 1 unit, 10x10x10 cm) were developed at Caltech with goal having a low cost fast be satellite [3]. The CubeSat form factor then widely used also scientific commercial space missions [4]. Alongside development nanosatellites, need better testing improving reliability [5]. As reported extensive study 855 [4], year 2018 almost 25% failed their early life stage (infant mortality). One subsystems more difficult tested is Attitude Determination Control System (ADCS). This subsystem includes sensors attitude determination, actuators control onboard controller. Integrated challenging task since device under test should freely rotate torque conditions sensors/actuators stimulated. A common way provide free rotational environment air bearing table [6].
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ژورنال
عنوان ژورنال: Materials research proceedings
سال: 2023
ISSN: ['2474-3941', '2474-395X']
DOI: https://doi.org/10.21741/9781644902677-30