Design of Attitude Control Systems for CubeSat‐Class Nanosatellite
We present a satellite attitude control system design using low‐cost hardware and software
for a 1U CubeSat. The attitude control system architecture is a crucial subsystem for any …
for a 1U CubeSat. The attitude control system architecture is a crucial subsystem for any …
Advanced fault detection and diagnosis in spacecraft attitude control systems: Current state and challenges
SH Pourtakdoust, M Fakhari Mehrjardi… - Proceedings of the …, 2023 - journals.sagepub.com
A review of advanced fault detection and diagnosis (FDD) techniques in attitude control
systems (ACSs) of spacecraft is presented. In the first part of the paper, several types of ACS …
systems (ACSs) of spacecraft is presented. In the first part of the paper, several types of ACS …
Attitude control experiment of a spinning spacecraft using only magnetic torquers
Magnetic torquers are attitude control devices used in spacecraft systems, and extensive
research has been conducted on the attitude control of such spacecraft systems equipped …
research has been conducted on the attitude control of such spacecraft systems equipped …
Magnetic plasma deorbit system for nano-and micro-satellites using magnetic torquer interference with space plasma in low Earth orbit
T Inamori, R Kawashima, P Saisutjarit, N Sako… - Acta astronautica, 2015 - Elsevier
We propose a magnetic plasma deorbit (MPD) system using magnetic torquers (MTQs) for
inducing the deorbit of nano-and micro-satellites. Currently, orbital space debris from these …
inducing the deorbit of nano-and micro-satellites. Currently, orbital space debris from these …
Spacecraft Attitude Testbed
M Stromecki, AB Younes - Advances in Space Research, 2024 - Elsevier
Spacecraft attitude determination and control systems (ADCS) stand as a pivotal factor for
ensuring the success of missions. As satellite sizes continue to decrease, the need for more …
ensuring the success of missions. As satellite sizes continue to decrease, the need for more …
[PDF][PDF] Magnetic actuators for nanosatellite attitude control
N Bellini - 2014 - core.ac.uk
The research and the activities presented in the following thesis report have been led at the
California Polytechnic State University (US) under the supervision of Prof. Jordi Puig Suari …
California Polytechnic State University (US) under the supervision of Prof. Jordi Puig Suari …
[PDF][PDF] The design, assembly, and testing of magnetorquers for a 1U CubeSat mission
J Amin, EG Lightsey - Georgia Institute of Technology, 2019 - ssdl.gatech.edu
A CubeSat is a miniaturized version of a satellite that is composed of cube units (U) of 10 cm
by 10 cm by 10 cm. Georgia Tech is developing several 1U CubeSats, the first of which is …
by 10 cm by 10 cm. Georgia Tech is developing several 1U CubeSats, the first of which is …
Power Saving in Magnetorquers by Operating in Cryogenic Environments
G Villalba-Alumbreros, D Lopez-Pascual… - Actuators, 2023 - mdpi.com
Satellites with cryogenic instrumentation have great potential for military, commercial, and
scientific space missions due to the increased sensitivity of their sensors, even for Low Earth …
scientific space missions due to the increased sensitivity of their sensors, even for Low Earth …
Attitude control system design & verification for CNUSAIL-1 with solar/drag sail
CNUSAIL-1, to be launched into low-earth orbit, is a cubesat-class satellite equipped with a
$2 m {\times} 2m $ solar sail. One of CNUSAIL's missions is to deploy its solar sail system …
$2 m {\times} 2m $ solar sail. One of CNUSAIL's missions is to deploy its solar sail system …
Parametric optimization and analysis of power efficient magnetorquer rod actuator for nanosatellite
CubeSats are popular nowadays due to their small size as well as low launch and
development costs. Also, they are getting popular as an Earth observation satellite. The …
development costs. Also, they are getting popular as an Earth observation satellite. The …