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

Author:

Busch S.,Bangert P.,Dombrovski S.,Schilling K.

Funder

Federal Ministry of Economics and Technology, Germany

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference14 articles.

1. P. Bangert, S. Busch, K. Schilling, Performance characteristics of the UWE-3 miniature attitude determination and control system, In: Proceedings of the 2nd IAA Conference on Dynamics and Control of Space Systems (DYCOSS), IAA-AAS-DyCoSS2-14-05-07, Rome, 2014.

2. R. Barza, Y. Aoki, K. Schilling, CubeSat UWE-1 technology tests and in orbit results, In: Proceedings of the 57th International Astronautical Congress Valencia, IAC-06-B5.3.07, 2006.

3. S. Busch, P. Bangert, K. Schilling, Attitude control demonstration for pico-satellite formation flying by UWE-3, In: Proceedings of the 4S-Symposium, Mallorca, 2014.

4. S. Busch, K. Schilling, Robust and efficient OBDH core module for the flexible picosatellite bus UWE-3, in: Proceedings of the 19th IFAC Symposium on Automatic Control In Aerospace, Würzburg, 2013, p. 218–223.

5. S. Busch, P. Bangert, F. Reichel, K. Schilling, The UWE satellite bus, a modular and flexible architecture for future picosatellite formations, in: Proceedings of the 64th IAC Congress, IAC-13.B4.6B.3, Beijing, China, 2013.

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