Publications

2015

• Modal Matching for LPV Model Reduction of Aeroservoelastic VehiclesTheis, J., Takarics, B., Pfifer, H., Balas, G. J. & Werner, H., 2 Jan 2015Electronic (full-text) versionResearch output: Contribution to conferences > Paper
• Updating a finite element based structural model of a small flexible aircraftGupta, A., Moreno, C. P., Pfifer, H., Taylor, B. & Balas, G. J., 2 Jan 2015Electronic (full-text) versionResearch output: Contribution to conferences > Paper
• Worst Case Analysis of a Saturated Gust Loads Alleviation SystemKnoblach, A., Pfifer, H. & Seiler, P. J., 2 Jan 2015Electronic (full-text) versionResearch output: Contribution to conferences > Paper
• Linear Parameter Varying Techniques Applied to Aeroservoelastic Aircraft: In Memory of Gary BalasPfifer, H., Moreno, C. P., Theis, J., Kotikapuldi, A., Gupta, A., Takarics, B. & Seiler, P., 2015, In:  IFAC-PapersOnLine. 48, 26, p. 103-108, 6 p.Electronic (full-text) versionResearch output: Contribution to journal > Research article

2014

• Low cost development of a nonlinear simulation for a flexible uninhabited air vehicleKotikalpudi, A., Moreno, C., Taylor, B., Pfifer, H. & Balas, G., Jun 2014, p. 2029-2034Electronic (full-text) versionResearch output: Contribution to conferences > Paper
• Structural model identification of a small flexible aircraftMoreno, C. P., Gupta, A., Pfifer, H., Taylor, B. & Balas, G. J., Jun 2014, p. 4379-4384Electronic (full-text) versionResearch output: Contribution to conferences > Paper

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
• 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

2012

• Quasi-LPV Model of a NDI-Controlled Missile Based on Function SubstitutionPfifer, H., 6 Sep 2012Electronic (full-text) versionResearch output: Contribution to conferences > Paper