UWE-3, in-orbit performance and lessons learned of a modular and flexible satellite bus for future pico-satellite formations

S Busch, P Bangert, S Dombrovski, K Schilling - Acta Astronautica, 2015 - Elsevier
Formations of small satellites offer promising perspectives due to improved temporal and
spatial coverage and resolution at reasonable costs. The UWE-program addresses in-orbit …

Perspectives for miniaturized, distributed, networked cooperating systems for space exploration

K Schilling - Robotics and Autonomous Systems, 2017 - Elsevier
Abstract Space exploration raises challenging autonomy requirements due to significant
signal propagation delays and data transmission interruptions in real-time critical situations …

Flight results of ESTCube-1 attitude determination system

A Slavinskis, H Ehrpais, H Kuuste, I Sünter… - Journal of Aerospace …, 2016 - ascelibrary.org
This paper presents the characterization and in-orbit validation of the ESTCube-1 attitude
determination system (ADS). ESTCube-1 is a one-unit CubeSat built by students and …

Fault Tolerant Attitude Estimation for Satellite at Low Earth Orbit*

H Henna, E Gasmi, H Toubakh, MR Kafi… - … on Control, Decision …, 2023 - ieeexplore.ieee.org
Maintaining an accurate estimate of the satellite's attitude is essential for pointing
performance to ensure the quality of products such as spatial images. Nevertheless, if …

[PDF][PDF] Advances in the Development of the Attitude Determination and Control System of the CubeSat MOVE-II

D Messmann, T Gruebler, F Coelho… - Proceedings of the 7th …, 2017 - academia.edu
Abstract MOVE-II (Munich Orbital Verification Experiment) will be the first CubeSat of the
Technical University of Munich (TUM) utilizing a magnetorquer-based active attitude …

[图书][B] Contributions to the Advance of the Integration Density of CubeSats

S Grau - 2019 - search.proquest.com
This thesis investigates potential technologies to increase the integration density of
CubeSats. Observations of the CubeSat market and missions are recorded in order to derive …

Advanced test environment for automated attitude control testing of fully integrated CubeSats on system level

O Ruf, M von Arnim, F Kempf, R Haber, L Elsner… - CEAS Space …, 2024 - Springer
As CubeSats are increasingly used for commercial purposes such as Earth observation,
communication, and scientific research, it is essential to improve their reliability. Recent …

[图书][B] MOVE-II-der zweite Kleinsatellit der Technischen Universität München

M Langer, N Appel, M Dziura, C Fuchs, P Günzel… - 2015 - researchgate.net
Der Lehrstuhl für Raumfahrttechnik (LRT) der Technischen Universität München (TUM)
beschäftigt sich seit dem Jahr 2006 mit der Entwicklung von Kleinsatelliten, sogenannten …

On-Orbit Magnetometer Data Calibration Using Genetic Algorithm and Interchangeability of the Calibration Parameters

DC Withanage, M Teramoto, M Cho - Applied Sciences, 2023 - mdpi.com
Magnetometers are important sensors with applications in the attitude determination and
control systems of satellites. CubeSats have certain limitations related to power, mass, and …

[图书][B] Software framework to support operations of nanosatellite formations

V Dombrovski - 2022 - opus.bibliothek.uni-wuerzburg.de
Since the first CubeSat launch in 2003, the hardware and software complexity of the
nanosatellites was continuosly increasing. To keep up with the continuously increasing …