| LPV model-based robust diagnosis of flight actuator faults A Varga, D Ossmann Control Engineering Practice 31, 135-147, 2014 | 55 | 2014 |
| Aeroservoelastic Modeling and Analysis of a Highly Flexible Flutter Demonstrator M Wuestenhagen, T Kier, YM Meddaikar, M Pusch, D Ossmann 2018 Atmospheric Flight Mechanics Conference, 3150, 2018 | 45 | 2018 |
| Diagnosis of actuator faults using LPV-gain scheduling techniques S Hecker, A Varga, D Ossmann AIAA Guidance, Navigation, and Control Conference, 2011 | 39 | 2011 |
| 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 | 36 | 2018 |
| Field testing of multi-variable individual pitch control on a utility-scale wind turbine D Ossmann, P Seiler, C Milliren, A Danker Renewable Energy 170, 1245-1256, 2021 | 35 | 2021 |
| Load reduction on a clipper liberty wind turbine with linear parameter‐varying individual blade pitch control D Ossmann, J Theis, P Seiler Wind Energy 20 (10), 1771-1786, 2017 | 33 | 2017 |
| Structured Control Design for a Highly Flexible Flutter Demonstrator M Pusch, D Ossmann, T Luspay Aerospace 6 (3), 27, 2019 | 32 | 2019 |
| Flight control design for a highly flexible flutter demonstrator T Luspay, D Ossmann, M Wuestenhagen, D Teubl, T Baár, M Pusch, ... AIAA Scitech 2019 Forum, 1817, 2019 | 32 | 2019 |
| Advanced sensor fault detection and isolation for electro-mechanical flight actuators D Ossmann, FLJ van der Linden | 29 | 2015 |
| Aeroelastic modeling and control of an experimental flexible wing M Pusch, D Ossmann, J Dillinger, TM Kier, M Tang, J Lübker AIAA scitech 2019 forum, 0131, 2019 | 25 | 2019 |
| Enhanced detection and isolation of angle of attack sensor faults D Ossmann, HD Joos AIAA Guidance, Navigation, and Control Conference, 2016 | 21 | 2016 |
| Detection and identification of loss of efficiency faults of flight actuators D Ossmann, A Varga 2013 Conference on Control and Fault-Tolerant Systems (SysTol), 19-24, 2013 | 21 | 2013 |
| -Optimal Blending of Inputs and Outputs for Modal Control M Pusch, D Ossmann IEEE Transactions on Control Systems Technology 28 (6), 2744-2751, 2019 | 20 | 2019 |
| Energetic approach for control surface disconnection fault detection in hydraulic aircraft actuators L Márton, D Ossmann Symposium on Fault Detection, Supervision and Safety for Technical Processes 12, 2012 | 20 | 2012 |
| Enhanced sensor monitoring to maintain optimal aircraft handling in case of faults D Ossmann, HD Joos, P Goupil Journal of Guidance, Control, and Dynamics 40 (12), 3127-3137, 2017 | 14 | 2017 |
| Fault detection and isolation of vehicle dynamics sensors and actuators for an overactuated X-by-wire vehicle LM Ho, D Ossmann 2014 IEEE 53rd Annual Conference on Decision and Control (CDC), 6560-6566, 2014 | 14 | 2014 |
| A fault diagnosis based reconfigurable longitudinal control system for managing loss of air data sensors for a civil aircraft⋆ A Varga, D Ossmann, HD Joos 19th IFAC World Congress, Cape Town, South Africa, 2014 | 14 | 2014 |
| LPV-model based identification approach of oscillatory failure cases A Varga, D Ossmann Symposium on Fault Detection, Supervision and Safety for Technical Processes 12, 2012 | 14 | 2012 |
| Fault tolerant control of an experimental flexible wing D Ossmann, M Pusch Aerospace 6 (7), 76, 2019 | 13 | 2019 |
| Baseline Flight Control System Design for an Unmanned Flutter Demonstrator D Ossmann, T Luspay, B Vanek Proceedings of the IEEE Aerospace Conference, Big Sky, MT, USA, 2019 | 13 | 2019 |
Manuel PuschProfessor, Munich University of Applied Sciences在 hm.edu 的电子邮件经过验证
