The attitude determination and control system of the picosatellite uwe-3

F Reichel, P Bangert, S Busch, K Ravandoor… - IFAC Proceedings …, 2013 - Elsevier
The picosatellite UWE-3 is the third generation of CubeSats at the University Würzburg. It is
equipped with all necessary satellite systems, among them an advanced attitude …

Hybrid attitude control on-board UWE-4 using magnetorquers and the electric propulsion system NanoFEEP

A Kramer, P Bangert, K Schilling - 2019 - digitalcommons.usu.edu
Orbit control on-board a 1U CubeSat was not demonstrated in orbit yet and is the technical
goal of the UWE-4 mission. For this purpose, the electric propulsion system NanoFEEP was …

Robust satellite engineering in educational cubesat missions at the example of the UWE-3 project

S Busch, K Schilling, P Bangert, F Reichel - IFAC Proceedings Volumes, 2013 - Elsevier
With the introduction of the cubesat standard hands-on satellite engineering received a
significant boost at educational university programs. However, not all missions could …

[图书][B] Design-und Verifikationstests des Lageerkennungs-und Lageregelungssystems für den Picosatelliten UWE-3

P Bangert, F Reichel, S Busch, K Schilling - 2012 - dglr.de
Zusammenfassung Das Picosatelliten-Programm der Universität Würzburg legt besonderes
Augenmerk auf die Durchführung von Tests schon während der Entwicklungsphase des …

[PDF][PDF] AGILE QUATERNION BASED ATTITUDE DETERMINATION AND CONTROL TO SUPPORT NEAR-SPACE VEHICLE OPERATIONS

F Mingireanu, L Baschir, S Miclos… - … SERIES A-APPLIED …, 2020 - scientificbulletin.upb.ro
Near-space is becoming more and more important both for space vehicle experimentation
and for Earth surveillance applications. Flight conditions in nearspace region emulate …