[PDF][PDF] Aerodynamic stability for CubeSats at ISS orbit
SA Rawashdeh, JE Lumpp - Journal of Small Satellites, 2013 - jossonline.com
At altitudes below 500 km, satellites experience a significant amount of aerodynamic drag
that can be utilized to stabilize satellites to align with the relative wind direction. Designing a …
that can be utilized to stabilize satellites to align with the relative wind direction. Designing a …
Development of an air-bearing testbed for nanosatellite attitude determination and control systems
PR Yanyachi, A Mamani-Saico, X Wang… - IEEE …, 2024 - ieeexplore.ieee.org
A testbed that simulates space conditions in a terrestrial laboratory is essential for
evaluating, verifying, and teaching attitude control in nanosatellites. The control …
evaluating, verifying, and teaching attitude control in nanosatellites. The control …
Attitude Analysis of Small Satellites Using Model‐Based Simulation
SA Rawashdeh - International Journal of Aerospace …, 2019 - Wiley Online Library
CubeSats, and small satellites in general, being small and relatively light, are sensitive to
disturbance torques in the orbital environment. We developed a simulation tool that includes …
disturbance torques in the orbital environment. We developed a simulation tool that includes …
An improved nanosatellite attitude control simulator for experimental research
A McCafferty-Leroux, A Newton… - Sensors and Systems …, 2023 - spiedigitallibrary.org
This paper details the design, fabrication, and development of an improved Nanosatellite
Attitude Control Simulator (NACS). The NACS consists of a mock 1U CubeSat (MockSat) …
Attitude Control Simulator (NACS). The NACS consists of a mock 1U CubeSat (MockSat) …
CommCube 1 and 2: A CubeSat series of missions to enhance communication capabilities for CubeSat
A Babuscia, B Corbin, R Jensen-Clem… - 2013 IEEE …, 2013 - ieeexplore.ieee.org
CubeSats and small satellites are becoming a way to explore space and to perform science
more affordably. As the goals for these spacecraft become more ambitious in terms of …
more affordably. As the goals for these spacecraft become more ambitious in terms of …
ProprioLogger: Evaluating Proprioception During Post-Surgical Rehabilitation using Portable IMUs
S Bellaire, A Abu–raddaha, K Zaka… - NAECON 2024-IEEE …, 2024 - ieeexplore.ieee.org
Proprioception is the sensation of body position and movement which is needed for balance
and the performance of coordinated complex movements. Pain or injury to the shoulder can …
and the performance of coordinated complex movements. Pain or injury to the shoulder can …
Performance analysis of passive magnetic pointing method for implementation of directional antennas on cubesats
JS Kang, JT King, CR Anderson… - International Journal of …, 2022 - Springer
As CubeSats have become hugely popular in the recent years, the demand on their
capability has also increased. As the missions and functionalities become more complex …
capability has also increased. As the missions and functionalities become more complex …
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 …
A stellar gyroscope for small satellite attitude determination
S Rawashdeh, J Lumpp Jr, J Barrington-Brown… - 2012 - digitalcommons.usu.edu
A stellar gyroscope is a star based attitude propagator that is capable of propagating a
spacecraft's attitude in three degrees of freedom by tracking the motion of the stars in an …
spacecraft's attitude in three degrees of freedom by tracking the motion of the stars in an …
Evaluation of solar array peak power tracking technologies for CubeSats
D Erb, S Rawashdeh, J Lumpp Jr - 2011 - digitalcommons.usu.edu
The increasing complexity and capability of small satellite missions is placing more stringent
requirements on spacecraft power systems. Higher power demands are usually met with …
requirements on spacecraft power systems. Higher power demands are usually met with …