Person

Fabian Binz

M. Sc.
Lehrstuhl und Institut für Flugsystemdynamik

Address

Building: 1320

Room: 502

Wüllnerstr. 7

52062 Aachen

Contact

workPhone
Phone: +49 241 80 96518
Fax: +49 241 80 92529

Office Hours

by appointment
 

Publications

Source Author(s)
[Contribution to a conference proceedings]
Attitude Control of Tiltwing Aircraft Using a Wing-Fixed Coordinate System and Incremental Nonlinear Dynamic Inversion
In: [10th International Micro-Air Vehicles Conference, IMAV2018, 2018-11-17 - 2018-11-23, Melbourne, Australia], 2018
Binz, Fabian
Islam, Tobias
Moormann, Dieter
[Contribution to a book, Contribution to a conference proceedings]
Nonlinear Model Predictive Flight Path Control of an Unmanned Powered Paraglider
In: Advances in Aerospace Guidance, Navigation and Control : Selected Papers of the Fourth CEAS Specialist Conference on Guidance, Navigation and Control held in Warsaw, 369-387, 2018
[DOI: 10.1007/978-3-319-65283-2_20]
Binz, Fabian
Hartmann, Philipp
Moormann, Dieter
[Contribution to a conference proceedings]
Auslegung und Implementierung eines zuverlässigen Kommunikationsnetzes für den sicheren Betrieb unbemannter Fluggeräte außerhalb der Sichtweite
In: Luft- und Raumfahrt - Hochtechnologie aus Deutschland : Deutscher Luft- und Raumfahrtkongress 2016 : 13.-15. September 2016, Braunschweig / DGLR, 1-5, 2016
Voget, Nicolai
Binz, Fabian
Dobrev, Yavor Ivanchev
Moormann, Dieter
[Conference Presentation]
Model Predictive Flightpath Control for an Unmanned Powered Paraglider
In: 10th AIRTEC 2015 München 2015-11-02 - 2015-11-05, 39 Folien : Illustrationen, grafische Darstellungen, 2015
Binz, Fabian
Hartmann, Philipp
Moormann, Dieter
 

Supervised Student Thesis

Type Title
bachelor thesis Time-Optimal Control without Overshoot of Stable 2nd Order Systems with Input Constraints
project thesis Wind Estimation for the Starting Procedure of a Tiltwing Aircraft
bachelor thesis Method for Estimation of Dynamic Derivatives using System Identification Based on Flight Test Data
master thesis Model Predictive Flight Path Control of an Unmanned Powered Paraglider
bachelor thesis Adaptive Heading Control of an Unmanned Powered Paraglider
bachelor thesis Design and Test of a MIMO Flight Controller with LQI Based Gain Feedback