This study presents a 3-Unit CubeSat design with commercial-off-the-shelf hardware,
Teflon®-fueled micropulsed plasma thrusters, and an attitude determination and control …

Large formations of satellites currently require extensive ground-based planning to enable
formation-wide collision-free reconfiguration. Allowing satellite formations the flexibility to …

Space technology for small satellites has made significant progress in the academic and
industrial fields, and an alternative focused on educational institutions is the CubeSat …

The CubeSat standard has inspired a new wave of engineers, researchers, and scientists–
all aiming to utilise „commercial off-the-shelf‟(COTS) subsystems to build nanosatellite …

Modern computers are now far in advance of satellite systems and leveraging of these
technologies for space applications could lead to cheaper and more capable spacecraft …

Most satellites are equipped with a gyroscope, allowing it to be used in dynamics
replacement mode for attitude estimation. However, gyroscopes have been known to fail …

Hardware and software architecture of a novel spacecraft Attitude Determination and Control
System (ADCS) based on smartphones using Variable Speed Control Moment Gyroscope …

II. Introduction ubeSats have emerged as platforms for various low earth orbit (LEO)
applications. Attitude control using propulsion requires the development of propulsive …

Abstract…… This study presents the overall design of a 3U CubeSat equipped with
commercial-off-the shelf hardware, Teflon-fueled micro-Pulsed Plasma Thrusters (µPPT) …

In this work, asymptotically stable state estimation schemes are proposed for rigid body
motion, using the framework of geometric mechanics. Rigorous stability analyses of the …