[HTML][HTML] Optimal Magnetorquer Rod Design for Small-Size Satellites using Axiomatic Design Theory and Nanocrystalline Material Core

LS Martins-Filho, MA Soares, E Gueron… - Journal of Aerospace …, 2024 - SciELO Brasil
The magnetic torquer rod, also called a magnetorquer, is the most popular actuator for
attitude control of satellites in low Earth orbit. In the case of nano and picosatellites, the …

Research on a rotational speed control strategy of the mandrel in a rotary steering system

L Zhang, G Zhang, J Spillian - Open Physics, 2018 - degruyter.com
Rotary steering systems are cutting-edge, intelligent oil drilling and steering equipment
developed at the end of the twentieth century. The core function of the bit pointing rotary …

[PDF][PDF] Orbital Dynamic Simulation and Passive Attitude Control of CubeSats

L Casaril, AG Brito - Journal of Space Technology, 2022 - larc.paginas.ufsc.br
This work reports the study of an orbital simulation used to analyze passive attitude control
systems of CubeSats. Such control system aims to guide the satellite's body without any …

Desenvolvimento de Torqueador Magnético para Controle de Atitude de CUBESAT Baseado na Teoria de Projeto Axiomático

MA Soares, LS Martins-Filho, E Gueron… - … de Automática-CBA, 2022 - sba.org.br
The article deals with the development of a magnetic torquer based on the axiomatic design
theory to define the constructive characteristics of the device to be applied in the attitude …

[PDF][PDF] Passive Attitude Stabilization of CubeSats in Low Earth Orbit

MTAS Ansari - 2021 - khalifauniversity.elsevierpure.com
Earth Orbit”, M. Sc. Thesis, M. Sc. in Mechanical Engineering, Department of Mechanical
Engineering, Khalifa University of Science and Technology, United Arab Emirates …