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Dr.-Ing. Zizung Yoon
Research fellow
Room: F 508
Phone: +49 30 314-24438
Email: query
Tasks
- Program manager of international master course "Master of Space Engineering"
- Research on spacecraft dynamics, satellite networks, satellite communication
- Lecturer of Spacecraft Dynamics & Control (until 2013)
- Supervision of theses
Projects
- Project management of project „S-band network for distributed satellites“ (project S Net)
- S-band transceiver for intersatellite communication of nano satellites (project SLink)
- Development, test and verification of attitude control system of small satellite DLR TET-1 (project TET-1)
- Reusable models for the virtual knowledgebased product development (project WieMod)
Education
2012 M.Sc. in Science Marketing, TU Berlin
2011 Ph.D. (Dr. -Ing.) in Aeronautics and Astronautics, TU Berlin
2006 Diploma Degree in Aeronautics and Astronautics, TU Berlin
Career
Seit 2010 Research fellow in the chair of space technology, TU Berlin
2006-2010 Engineer within project TET-1 und project WieMod at Astro- und Feinwerktechnik Adlershof GmbH
2006 Space System Research Lab. Korea Aerospace Univ. (internship)
| Citation key | kirchner.2013.IWLR.Laser |
|---|---|
| Author | Kirchner, Georg; Grunwaldt, Ludwig; Neubert, Reinhard; Koidl, Franz; Barschke, Merlin; Yoon, Zizung and Fiedler, Hauke |
| Title of Book | Proceedings of the 18th International Workshop on Laser Ranging |
| Year | 2013 |
| Address | Fujiyoshida, Japan |
| Month | November |
| Abstract | Several small satellites in the class of pico- and nano-satellites will be equipped with multiple small corner cubes: OPS-SAT (ESA), S-Net and TechnoSat (8 kg resp. 15 kg; Technical University Berlin). The size of these satellites is in the range of 10x10x30 cm, up to about 40 x 40 x 30 cm; the planned circular orbits are in the 500 - 600 km range. Commercially available 0.5” corner cubes will be used for SLR; a single corner cube of this size will be sufficient for SLR to the planned LEO orbits. Placing several of these corner cubes on each side of the satellites will not only allow for standard SLR and POD, but also for an independent attitude determination with < 1° accuracy, even after the end of the satellites lifetime, or in case of problems or satellite failure. |