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A comprehensive review on CubeSat electrical power system architectures
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 …
easier deployment. The electrical power system (EPS) is one of the significant subsystems …
A review of balancing methods for satellite simulators
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 …
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
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 …
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 …
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
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 …
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 …
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 …
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 …
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 …
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 …
vector aiding a low-cost IMU. CubeSats provide relatively cost-effective methods of …