Daniel Ossmann
Daniel Ossmann
Professor @ Munich University of Applied Sciences HM
Verified email at - Homepage
Cited by
Cited by
LPV model-based robust diagnosis of flight actuator faults
A Varga, D Ossmann
Control Engineering Practice 31, 135-147, 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
Diagnosis of actuator faults using LPV-gain scheduling techniques
S Hecker, A Varga, D Ossmann
AIAA Guidance, Navigation, and Control Conference, 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
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
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
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
Structured Control Design for a Highly Flexible Flutter Demonstrator
M Pusch, D Ossmann, T Luspay
Aerospace 6 (3), 27, 2019
Advanced sensor fault detection and isolation for electro-mechanical flight actuators
D Ossmann, FLJ van der Linden
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
-Optimal Blending of Inputs and Outputs for Modal Control
M Pusch, D Ossmann
IEEE Transactions on Control Systems Technology 28 (6), 2744-2751, 2019
Enhanced detection and isolation of angle of attack sensor faults
D Ossmann, HD Joos
AIAA Guidance, Navigation, and Control Conference, 2016
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
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
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
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
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
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
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
Fault tolerant control of an experimental flexible wing
D Ossmann, M Pusch
Aerospace 6 (7), 76, 2019
The system can't perform the operation now. Try again later.
Articles 1–20