| Robustness analysis of linear parameter varying systems using integral quadratic constraints H Pfifer, P Seiler International Journal of Robust and Nonlinear Control 25 (15), 2843-2864, 2015 | 94 | 2015 |
| Robust control design for active flutter suppression J Theis, H Pfifer, PJ Seiler AIAA Atmospheric Flight Mechanics Conference, 1751, 2016 | 93 | 2016 |
| Robust synthesis for linear parameter varying systems using integral quadratic constraints S Wang, H Pfifer, P Seiler Automatica 68, 111-118, 2016 | 67 | 2016 |
| Generation of optimal linear parametric models for LFT-based robust stability analysis and control design H Pfifer, S Hecker IEEE Transactions on Control Systems Technology 19 (1), 118-131, 2010 | 61 | 2010 |
| Integral quadratic constraints for delayed nonlinear and parameter-varying systems H Pfifer, P Seiler Automatica 56, 36-43, 2015 | 58 | 2015 |
| Less conservative robustness analysis of linear parameter varying systems using integral quadratic constraints H Pfifer, P Seiler International Journal of Robust and Nonlinear Control 26 (16), 3580-3594, 2016 | 54 | 2016 |
| Robust modal damping control for active flutter suppression J Theis, H Pfifer, P Seiler Journal of Guidance, Control, and Dynamics 43 (6), 1056-1068, 2020 | 41 | 2020 |
| Robust autopilot design for landing a large civil aircraft in crosswind J Theis, D Ossmann, F Thielecke, H Pfifer Control Engineering Practice 76, 54-64, 2018 | 37 | 2018 |
| Modal matching for LPV model reduction of aeroservoelastic vehicles J Theis, B Takarics, H Pfifer, GJ Balas, H Werner AIAA Atmospheric Flight Mechanics Conference, 1686, 2015 | 33 | 2015 |
| System Identification of a small flexible aircraft-invited H Pfifer, BP Danowsky AIAA Atmospheric Flight Mechanics Conference, 1750, 2016 | 32 | 2016 |
| Unsteady aerodynamics modeling for a flexible unmanned air vehicle A Kotikalpudi, H Pfifer, GJ Balas AIAA Atmospheric Flight Mechanics Conference, 2854, 2015 | 28 | 2015 |
| Updating a finite element based structural model of a small flexible aircraft A Gupta, CP Moreno, H Pfifer, B Taylor, GJ Balas AIAA Modeling and Simulation Technologies Conference, 0903, 2015 | 27 | 2015 |
| Control-oriented system and parameter identification of a small flexible flying-wing aircraft BP Danowsky, DK Schmidt, H Pfifer AIAA Atmospheric Flight Mechanics Conference, 1394, 2017 | 22 | 2017 |
| Structural model identification of a small flexible aircraft CP Moreno, A Gupta, H Pfifer, B Taylor, GJ Balas 2014 American Control Conference, 4379-4384, 2014 | 20 | 2014 |
| Linear parameter varying techniques applied to aeroservoelastic aircraft: In memory of Gary Balas H Pfifer, CP Moreno, J Theis, A Kotikapuldi, A Gupta, B Takarics, P Seiler IFAC-PapersOnLine 48 (26), 103-108, 2015 | 18 | 2015 |
| LPV/LFT Modeling and its Application in Aerospace H Pfifer Verlag Dr. Hut, 2013 | 18 | 2013 |
| LPV controller synthesis for a generic missile model H Pfifer, S Hecker 2010 IEEE International Conference on Control Applications, 1838-1843, 2010 | 17 | 2010 |
| Worst case gain computation of linear time-varying systems over a finite horizon F Biertümpfel, H Pfifer 2018 IEEE Conference on Control Technology and Applications (CCTA), 952-957, 2018 | 15 | 2018 |
| Integrated flight control design for a large flexible aircraft J Theis, H Pfifer, G Balas, H Werner 2015 American Control Conference (ACC), 3830-3835, 2015 | 15 | 2015 |
| Applied LPV control exploiting the separation principle for the single axis positioning of an industrial manipulator F Saupe, H Pfifer 2011 IEEE International Conference on Control Applications (CCA), 1476-1481, 2011 | 15 | 2011 |
Peter Seiler JrUniversity of Michigan, Ann ArborBestätigte E-Mail-Adresse bei umich.edu
