Results 91 to 100 of about 7,433 (210)
Corrections to “On-Board Computer for CubeSats: State-of-the-Art and Future Trends”
Presents corrections to the paper, (On-Board Computer for CubeSats: State-of-the-Art and Future Trends)
Angela Cratere +4 more
doaj +1 more source
Survey of Propulsion Technologies Applicable to Cubesats
At present, no Cubesat has flown in space featuring propulsion. This was acceptable as long as CubeSats were flown mostly as university experiments.
Ziemer, John +2 more
core
Propulsion System and Orbit Maneuver Integration in CubeSats: Trajectory Control Strategies Using Micro Ion Propulsion [PDF]
The Propulsion System and Orbit Maneuver Integration in CubeSats project aims to solve the challenges of integrating a micro electric propulsion system on a CubeSat in order to perform orbital maneuvers and control attitude.
Petro, Andrew +2 more
core
Design and Analysis of Optical Telescope Subsystem
In the realm of space exploration, there is a notable upsurge in advanced remote imaging systems, particularly in CubeSats, owing to their efficiency and increasing payload capacities.
Alper Şanlı, Tuncay Yunus Erkeç
doaj
On-Board Image Enhancement on Remote Sensing Payload
CubeSats are designed to optimize applications within the strict constraints of space and power. This paper presents an On-Board Image Enhancement technique for remote sensing payloads, focusing on achieving Auto White Balance (AWB) with limited ...
Guo-Cheng Xu +4 more
doaj +1 more source
Comprehensive analysis of Cubesat electrical power systems for efficient energy management
The new space movement has seen a rise since the last decade, thanks to CubeSats, which are affordable with fast development times and ease of deployment.
Usama Shakoor +2 more
doaj +1 more source
Celestial Bodies Far-Range Detection with Deep-Space CubeSats. [PDF]
Franzese V, Topputo F.
europepmc +1 more source
Assisted Snapshot GNSS Position, Navigation, and Timing for LEO Satellites. [PDF]
Kim S +4 more
europepmc +1 more source
Impact observations of asteroid Dimorphos via Light Italian CubeSat for imaging of asteroids (LICIACube). [PDF]
Dotto E, Zinzi A.
europepmc +1 more source
Mission Objective: Design and assemble a small, autonomous 1U CubeSat measuring instrument, weighing up to 1,500 grams and measuring 105 mm x 105 mm x 105 mm (L x H x W), capable of conducting atmospheric research, aerial photography, and safe return to Earth.
openaire +1 more source

