1. An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit;Azari,2016
2. Bernard, N., Maisonobe, L., Barbulescu, L., Bazavan, P., Scortan, S., Cefola, P.J., Casasco, M., Merz, K., 2015. Validating short periodics contributions in a draper semi-analytical aatellite theory implementation: the orekit example. In: 25th International Symposium on Space Flight Dynamics.
3. Boain, R.J., 2004. A-b-cs of sun-synchronous orbit mission desing. In: 14th AAS/AIAA Space Flight Mechanics Conference, AAS/AIAA.
4. Bock, D., Kramer, A., Bangert, P., Schilling, K., Tajmar, M., 2015. Nanofeep on uwe platform - formation flying of cubesats using miniaturized field emission electric propulsion thrusters. In: Joint Conference of 30th ISTS, 34th IEPC and 6th NSAT.
5. Solution of the problem of artificial satellite theory without drag;Brouwer;Astron. J.,1959