479.575 PEOPLE
People | Locations | Statistics |
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Ziakopoulos, Apostolos | Athens |
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Vigliani, Alessandro | Turin |
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Catani, Jacopo | Rome |
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Statheros, Thomas | Stevenage |
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Utriainen, Roni | Tampere |
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Guglieri, Giorgio | Turin |
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Martínez Sánchez, Joaquín |
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Tobolar, Jakub |
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Volodarets, M. |
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Piwowar, Piotr |
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Tennoy, Aud | Oslo |
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Matos, Ana Rita |
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Cicevic, Svetlana |
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Sommer, Carsten | Kassel |
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Liu, Meiqi |
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Pirdavani, Ali | Hasselt |
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Niklaß, Malte |
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Lima, Pedro | Braga |
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Turunen, Anu W. |
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Antunes, Carlos Henggeler |
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Krasnov, Oleg A. |
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Lopes, Joao P. |
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Turan, Osman |
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Lučanin, Vojkan | Belgrade |
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Tanaskovic, Jovan |
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Voskuijl, Mark
Netherlands Defence Academy
in Cooperation with on an Cooperation-Score of 37%
Topics
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- aircraft
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- comfort
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- architecture
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- control system
- pressure
- transient
- aerodynamic
- system architecture
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- industry
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- flight test
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- show 71 more
Publications (38/38 displayed)
- 2021A Control Allocation approach to induce the center of pressure position and shape the aircraft transient responsecitations
- 2020Active and passive camber morphing for helicopter rotors towards performance improvements in hover and vertical flight
- 2019A Thrust-Elevator Interaction Criterion for Aircraft Optimal Longitudinal Controlcitations
- 2019Streamlining Cross-Organizational Aircraft Development: Results from the AGILE Projectcitations
- 2018Helicopter drive train load alleviation in hover by nonlinear control
- 2018Hoplite - a conceptual design environment for helicopters incorporating morphing rotor technology
- 2018Analysis and design of hybrid electric regional turboprop aircraftcitations
- 2018Helicopter main rotor hub load alleviation using a variable incidence horizontal stabilizer
- 2018Aerodynamic installation effects of lateral rotors on a novel compound helicopter configuration
- 2017An approach to estimate aircraft touchdown attitudes and control inputscitations
- 2016Helicopter main rotor hub load alleviation using a variable incidence horizontal stabilizer
- 2016Mechatronic Design and Optimization Using Knowledge-Based Engineering Applied to an Inherently Unstable and Unmanned Aerial Vehiclecitations
- 2015The impact of control allocation on trim drag of blended wing body aircraftcitations
- 2015Condition-based flight control for helicopters: An extension to condition-based maintenancecitations
- 2014Control development of a simplified aircraft model to study the GABRIEL concept. Deliverable 4.5
- 2014Test concept development of the GABRIEL concept, Deliverable 4.7
- 2014Evaluation of the simulation results of the GABRIEL concept. Deliverable 4.3
- 2014DETERMINATION OF REPRESENTATIVE LOADING CONDITIONS FOR EFFECTIVE SEMITRAILER DESIGNcitations
- 2013Improving structural weight estimation of novel aircraft configurations to enhance flying quality analysis
- 2013Knowledge Based Engineering to Support Automotive Conceptual Design and Automatic Control Software Developmentcitations
- 2013Control allocation performance for blended wing body aircraft and its impact on control surface designcitations
- 2013Simulation technology and simulation of the GABRIEL concept, Deliverable 4.2
- 2013Conceptual design of a magnetic-assisted take-off system for mid-range transport aircraft
- 2013Take-off and landing performance of the aircraft using the GABRIEL concept, Deliverable 3.8
- 2012Conceptual Design of a Magnetic-Assisted Take-off System for Mid-Range Transport Aircraft
- 2011Environmental impact evaluation of aircraft at system-of-systems levelcitations
- 2011Addressing complexity in sustainable aircraft designcitations
- 2011Implementation of a Heterogeneous, Variable-Fidelity Framework for Flight Mechanics Analysis in Preliminary Aircraft Design
- 2010Simulation of automatic helicopter deck landings using nature inspired flight controlcitations
- 2008Helicopter load alleviation using active controlcitations
- 2008Nonlinear attitude control laws for the Bell 412 helicoptercitations
- 2008Controllability of blended wing body aircraft
- 2007Low-speed control of tiltrotor aircraft using H-infinity
- 2007Flight test of a nonlinear control law on the bell 412 advanced systems research aircraft
- 2007Active control of flight path and critical loads in tilt-rotor aircraft
- 2007Modelling, design and rapid prototyping of control laws for the Bell-412 advanced systems research aircraft
- 2006Multivariable control of the bell 412 helicopter
- 2005Helicopter flight control law design using H∞ techniquescitations
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