Attitude Control of a Nanosatellite Using Only Magnetic Torquers
نویسندگان
چکیده
منابع مشابه
Distributed attitude synchronization control for a group of flexible spacecraft using only attitude measurements
This paper considers the problem of attitude synchronization control of a group of flexible spacecraft under an undirected communication graph and in the absence of measurements of both modal variables and spacecraft angular velocities. To solve this problem, a nonlinear observer is introduced to estimate the unmeasurable modal variables and spacecraft angular velocities. Then, the backstepping...
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15 صفحه اولA Novel Adaptive Unscented Kalman Filter Attitude Estimation and Control System for a 3U Nanosatellite
A novel adaptive unscented Kalman filter (AUKF) based estimation algorithm is proposed for a 3U Cubsat. This small satellite employs a three axis magnetometer and three MEMS gyroscopes as well as three magnetic torque rods and one reaction wheel on the pitch axis. Unlike the existing UKF, in this paper, an n+1 sigma set is used to estimate the nanosatellite attitude instead of 2n + 1 sigma poin...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
سال: 2018
ISSN: 1884-0485
DOI: 10.2322/tastj.16.441