Abstract The Micro-sized Microwave Atmospheric Satellite (MicroMAS) is a dual-spinning 3U
CubeSat equipped with a nine-channel passive microwave spectrometer observing near the …

This study is aimed at addressing the practical challenges of conducting hardware-in-the-
loop simulation (HILS) for a CubeSat attitude determination and control system (ADCS) with …

Algorithms for the angular motion determination of a nanosatellite based on the extended
Kalman filter using measurements of onboard solar sensors, a magnetometer, and an …

In recent years, there has been an increase in the number of small satellites that have been
made and launched into space. An important part of the technology needed to make these …

This paper considers the problem of determining the position of the center-of-mass and
inertia tensor of a microsatellite mockup on an air-bearing testbed by using optical …

Current attitude determination and control system simulation platforms for nanosatellites are
typically not capable of undergoing continuous rotation about all three axes. Continuous …

The design and test of a 6U CubeSat Attitude Determination and Control System (ADCS) are
explored to establish single-axis control using AFIT's CubeSat testbed consisting of a …

АННОТАЦИЯ на диссертацию «Математическое моделирование и компьютерное
моделирование динамического поведения наноспутников на орбите», которую …

В работе рассматривается задача определения положения центра масс и тензора
инерции макета на аэродинамическом подвесе по измерениям оптической системы …

摘要(中) 本研究開發一個能讓衛星在地面上, 模擬太空中磁場變化的磁場模擬艙. 磁場模擬艙,
要能抵銷機構誤差所造成的雜訊, 還能抵抗外來環境磁場變化所帶來的干擾 …