Progress Towards Controlled Re-entry and Recovery of CubeSats
FW Downey - 2023 - espace.curtin.edu.au
The primary objective of this work was to progress towards performing controlled re-entry
and recovery missions using CubeSats to increase the frequency of Solar System …
and recovery missions using CubeSats to increase the frequency of Solar System …
Studies on the Functionality of On-Board Computer in 1U CubeSat
N Anusha, M Fardeen, K Chandana… - … on Circuit Power …, 2023 - ieeexplore.ieee.org
The paper studies the various functionality of the On-Board Computer (OBC) used in 1U
CubeSat for Leo orbit. The OBC in CubeSat is responsible for controlling and managing all …
CubeSat for Leo orbit. The OBC in CubeSat is responsible for controlling and managing all …
Taking Advantage of Geomagnetic Storms for B-Dot Attitude Control in Small Satellites
AT Balkir, D Cilden-Guler - Journal of Aeronautics and Space …, 2024 - jast.hho.msu.edu.tr
The geomagnetic field models are presented with the external field influences taken into
account. Magnetometers detect the external field, although most geomagnetic field models …
account. Magnetometers detect the external field, although most geomagnetic field models …
[PDF][PDF] Aerodynamic Satellite Attitude Control in Very Low Earth Orbit
C Chang, R Breidenthal, BC Lin, YX Yang - 2024 - researchgate.net
Simulation of a 3U-sized standard platform with four control panels attached to the rear part
of the satellite at an altitude of 300 km was performed in Simulink to verify the feasibility of …
of the satellite at an altitude of 300 km was performed in Simulink to verify the feasibility of …
Development of a MATLAB tool for Automated Calculation of CubeSat Budgets with Margins
E Hoxha - 2023 - webthesis.biblio.polito.it
A generic mission analysis system that will simulate orbit and attitude based on a range of
values for parameters (power, volume, size, data) instead of fixed values. The end result is a …
values for parameters (power, volume, size, data) instead of fixed values. The end result is a …
[PDF][PDF] Study and Implementation of On-Board Computer Functionality in 1U CubeSat
N Anusha, M Fardeen, K Chandana, M Abdullah… - researchgate.net
On-Board Computer (OBC) used in 1U (unit) CubeSat for Leo orbit. The OBC in CubeSat is
responsible for controlling and managing all the subsystems of the Spacecraft. The …
responsible for controlling and managing all the subsystems of the Spacecraft. The …