A comprehensive review on CubeSat electrical power system architectures

A Edpuganti, V Khadkikar, MS El Moursi… - … on power electronics, 2021 - ieeexplore.ieee.org
CubeSats have been popular for space research due to lower cost, faster development, and
easier deployment. The electrical power system (EPS) is one of the significant subsystems …

A review of balancing methods for satellite simulators

RC da Silva, RA Borges, S Battistini, C Cappelletti - Acta astronautica, 2021 - Elsevier
This article presents a general review of the existing methods for balancing satellite
simulators. The mathematical modeling for the kinematics and the dynamics of the satellite …

Automatic mass balancing system for a dynamic CubeSat attitude simulator: development and experimental validation

A Bahu, D Modenini - CEAS Space Journal, 2020 - Springer
This paper describes the automatic balancing and inertia identification system for three
degrees of freedom CubeSat attitude simulator testbed. For a reliable verification of the …

CubeSat technology past and present: Current state-of-the-art survey

BMM Bomani - 2021 - ntrs.nasa.gov
A cube satellite (CubeSat) is an evolving and emerging technology that gives a novice or
advanced researcher relatively affordable access to space research experiments and …

Multi-Agent Passive Inspection Coverage of an Unknown Torque-Free Rigid Body Using Monte Carlo Analysis and Quaternion Measurements

SC Cutlip, J Aurand, K Lang, S Phillips - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
This paper considers the problem of determining agent positions from which to perform a
multi-agent inspection of an unknown RSO (resident space object) that is freely tumbling …

Nanosatellite Design Considerations for a Mission to Explore the Propellant Sloshing Problem

M Fogel, S Sushil Mishra, L Burlion - Journal of Spacecraft and Rockets, 2024 - arc.aiaa.org
Sloshing Platform for In-Orbit Controller Experimentation is an ambitious, student run
mission to design and fly a cubesat to study fluid sloshing in spacecraft. The project will …

Gyroless spin-stabilization controller and deorbiting algorithm for cubesats

JE Morales, J Kim, RR Richardson - International Journal of Aeronautical …, 2021 - Springer
CubeSats are becoming increasingly popular in the scientific community. While they provide
a whole new range of opportunities for space exploration, they also come with their own …

Nanosatellite Design Considerations for a Mission to Explore the Propellant Sloshing Problem

SS Mishra, L Burlion - arxiv preprint arxiv:2412.20659, 2024 - arxiv.org
Sloshing Platform for In-Orbit Controller Experimentation is an ambitious, student run
mission to design and fly a cubesat to study fluid sloshing in spacecraft. The project will …

[PDF][PDF] Attitude Determination and Control of Thinsat System Using Adaptive Control Technique

UI Christian, EI Ifeanyichukwu… - Engineering Science, 2023 - researchgate.net
This paper presents attitude determination and control of ThinSat system using an adaptive
control technique. This study aims to reduce the impact of dynamic torque on the angular …

Single-Vector Aiding of an IMU for CubeSat Attitude Determination

KP Laughlin - 2020 - search.proquest.com
This thesis examines CubeSat attitude determination using the Earth's magnetic field (EMF)
vector aiding a low-cost IMU. CubeSats provide relatively cost-effective methods of …