Results 91 to 100 of about 7,433 (210)

Corrections to “On-Board Computer for CubeSats: State-of-the-Art and Future Trends”

open access: yesIEEE Access
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

open access: yes, 2010
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]

open access: yes, 2015
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

open access: yesHavacılık ve Uzay Teknolojileri Dergisi
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

open access: yesAerospace
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

open access: yesDiscover Energy
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

Development of the 1U CubeSat

open access: yes
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

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