Flightplan Flight Tests of an Experimental DA42 General Aviation Aircraft

被引:0
|
作者
Schatz, Simon P. [1 ]
Schneider, Volker [1 ]
Karlsson, Erik [1 ]
Holzapfel, Florian [1 ]
Baier, Thaddaeus [1 ]
Doerhoefer, Christoph [1 ]
Hochstrasser, Markus [1 ]
Gabrys, Agnes [1 ]
Krause, Christoph [1 ]
Lauffs, Patrick J. [1 ]
Mumm, Nils C. [1 ]
Nuernberger, Kajetan [1 ]
Peter, Lars [1 ]
Spiegel, Philip [1 ]
Steinert, Lukas [1 ]
Zollitsch, Alexander W. [1 ]
机构
[1] Tech Univ Munich, Inst Flight Syst Dynam, D-85748 Garching, Germany
关键词
TRACKING;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The recent emergence of unmanned aerial vehicles asked for both well-performing auto-flight systems and fly-bywire architectures. Towards this end, the trajectory control module of an integrated auto-flight control system is introduced in this paper, which utilizes nonlinear second-order error dynamics of the position error and uses nonlinear dynamic inversion as a control methodology. Flight test results of a flightplan mission conducted on the institute's general aviation aircraft - a DA42 augmented with experimental fly-by-wire - are presented and the controller's performance is evaluated.
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页数:6
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