Publications

2014

• Development and Testing of a CubeSat with Highly Miniaturised FEEP Thrusters on a Thrust Balance with Sub-Nanonewton ResolutionBock, D., Rössler, F., Kössling, M. & Tajmar, M., 2014, Proceedings of the 65th International Astronautical Congress. TorontoResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• Development and Testing of Field Emission Thrusters at TU DresdenBock, D., Ebert, M., Rössler, F., Kössling, M. & Tajmar, M., 2014, Proceedings of the 5th Russian-German Conference on Electric Propulsion. Dresden, September 7-12, 16 p.Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• MEMS-Based Gas-Field-Ion-Source for Micro-Thruster and Gas Sensor ApplicationTajmar, M. & Stämm, S., 2014, Proceedings of the 4th Spacecraft Propulsion Conference. Cologne, May 19-22Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• Proceedings of the SMART Rockets Project: Development of a Sounding Rocket and the Corresponding Ground Support EquipmentBach, C., Sieder, J., Grasselt-Gille, S., Przybilski, O. & Tajmar, M., 2014, Proceedings of the 63rd German Aerospace Congress (DGLR). Augsburg, Sept. 16-18Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• Simulation of the Impact Behavior of Polymer WindshieldsMarkmiller, J., 2014, Crash Colloquium DLR Stuttgart. StuttgartResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution

2013

• Robust performance analysis: A review of techniques for dealing with infinite dimensional LMIsKnoblach, A., Assanimoghaddam, M., Pfifer, H. & Saupe, F., Aug 2013, p. 972-977Electronic (full-text) versionResearch output: Contribution to conferences > Paper
• Development of a Highly Precise Micro-Newton Thrust BalanceHey, F., Keller, A., Papendorf, D., Braxmaier, C., Tajmar, M., Johann, U. & Weise, D., 2013, Proceedings of the 33rd International Electric Propulsion Conference. Washington DC, Oct. 6-10Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• Impact behavior of monolithic and multi-layered polymer windshields for light helicoptersMarkmiller, J. & Burger, U., 2013, 69th American Helicopter Society Annual Forum, USA. Phoenix, Arizona, 21.05.-23.05.2013Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• LFT Model Generation via ℓ1-Regularized Least SquaresPfifer, H. & Hecker, S., 2013, Advances in Aerospace Guidance, Navigation and Control. Chu, Q., Mulder, B., Choukroun, D., van Kampen, E., de Visser, C. & Looye, G. (eds.). Springer, Berlin [u. a.], p. 85-98, Chapter 7Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Chapter in book/Anthology/Report
• Linear Parameter Varying Control of an Agile Missile Model Based on the Induced L 2-norm FrameworkTekin, R. & Pfifer, H., 2013, Advances in Aerospace Guidance, Navigation and Control. Chu, Q., Mulder, B., Choukroun, D., van Kampen, E., de Visser, C. & Looye, G. (eds.). Springer, Berlin [u. a.], p. 3-14, Chapter 1Electronic (full-text) versionResearch output: Contribution to book/conference proceedings/anthology/report > Chapter in book/Anthology/Report