380.256 PEOPLE
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| Seuring, Stefan |
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| Nor Azizi, S. |
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| Pato, Margarida Vaz |
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| Kölker, Katrin |
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| Huber, Oliver |
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| Király, Tamás |
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| Spengler, Thomas Stefan |
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| Al-Ammar, Essam A. |
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| Dargahi, Fatemeh |
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| Mota, Rui |
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| Mazalan, Nurul Aliah Amirah |
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| Macharis, Cathy | Brussels |
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| Arunasari, Yova Tri |
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| Nunez, Alfredo | Delft |
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| Bouhorma, Mohammed |
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| Bonato, Matteo |
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| Fitriani, Ira |
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| Autor Correspondente Coelho, Sílvia. |
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| Pond, Stephen |
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| Okwara, Ukoha Kalu |
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| Toufigh, Vahid |
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| Campisi, Tiziana | Enna |
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| Ermolieva, Tatiana |
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| Sánchez-Cambronero, Santos |
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| Agzamov, Akhror |
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Looye, Gertjan
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (36/36 displayed)
- 2022Tilt-Wing Control Design for a Unified Control Conceptcitations
- 2022Dynamic Modeling and Analysis of Tilt-Wing Electric Vertical Take-Off and Landing Vehiclescitations
- 2021Aircraft Mission Simulation with the updated FlightDynamics Library
- 2020Aircraft Mission Simulation Framework for Loads Analysiscitations
- 2020Active Flutter Mitigation Testing on the FLEXOP Demonstrator Aircraftcitations
- 2020Active Flutter Mitigation Testing on the FLEXOP Demonstrator Aircraftcitations
- 2020Flight Testing a Linear Parameter Varying Control Law on a Passenger Aircraftcitations
- 2020Design and evaluation of advanced intelligent flight controllerscitations
- 2020Analysis of Automatic Control Function Effects on Vertical Tail Plane Critical Load Conditionscitations
- 2019Multi-Domain Flight Simulation with the DLR Robotic Motion Simulatorcitations
- 2019Flight testing of incremental backstepping based control laws with angular accelerometer feedbackcitations
- 2019Design and Verification of a Linear Parameter Varying Control Law for a Transport Aircraft
- 2019An Integrated Analysis Model for Assessment of Critical Load Conditions for the Vertical Tail Plane
- 2018A Rapid-prototyping process for Flight Control Algorithms for Use in over-all Aircraft Designcitations
- 2018Aircraft control using actuator current
- 2016An innovative route from wind tunnel experiments to flight dynamics analysis for a highly swept flying wingcitations
- 2016Design and Piloted Simulator Evaluation of Adaptive Safe Flight Envelope Protection Algorithmcitations
- 2013Generic TECS based autopilot for an electric high altitude solar powered aircraft
- 2013A Constrained Inverse Modeling Approach for Trajectory Optimizationcitations
- 2013Design and flight testing of nonlinear autoflight control laws incorporating direct lift controlcitations
- 2013Modular scalable system for operation and testing of UAVscitations
- 2013TECS/THCS-based generic autopilot control laws for aircraft mission simulation
- 2012Integrated Simulation Models for High-Altitude Solar-Powered Aircraftcitations
- 2011The Parametric Aircraft Noise Analysis Module - status overview and recent applications
- 2011Flyover Noise Measurements of a Spiraling Noise Abatement Approach Procedurecitations
- 2010GBAS Based Autoland System: A Bottom Up Approach for GAST-D Requirementscitations
- 2010Flyover Noise Measurements of a Spiraling Noise Abatement Approach Procedure
- 2008The New CLR Flight Dynamics Library
- 2008Development of a generic GUI-based software environment for aircraft trimming
- 2008An Integrated Approach to Aircraft Modelling and Flight Control Law Design
- 2007Process, methods and tools for flexible aircraft flight dynamics model integration
- 2006Design of Autoland Controller Functions with Multiobjective Optimization
- 2005Development of Aircraft Flight Loads Analysis Models with Uncertainties for Pre-Design Studies
- 2005Multi-Disciplinary Aircraft Model Development Using Object-Oriented Modelling Techniques
- 2005Comparison of Model Integration Approaches for Flexible Aircraft Flight Dynamics Modelling
- 2001Design of Robust Dynamic Inversion Control Laws using Multi-Objective Optimization
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