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Published in 2017 at "Aircraft Engineering and Aerospace Technology"
DOI: 10.1108/aeat-09-2015-0214
Abstract: Purpose The purpose of this paper is to identify the flexible aircraft model accurately from the frequency responses. Design/methodology/approach The frequency domain output error method is used to estimate the aerodynamic (rigid body and elastic…
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Keywords:
aircraft;
flexible aircraft;
identification;
frequency domain ... See more keywords
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Published in 2018 at "Journal of Aircraft"
DOI: 10.2514/1.c034684
Abstract: A nonlinear modeling strategy is introduced to drive online optimization-based controllers for trajectory tracking and stabilization of very flexible aircraft. This is achieved thanks to a compact ...
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Keywords:
aircraft;
aeroelastic control;
nonlinear aeroelastic;
control flexible ... See more keywords
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Published in 2019 at "Journal of Guidance, Control, and Dynamics"
DOI: 10.2514/1.g003980
Abstract: This paper designs an incremental nonlinear dynamic inversion control law for free-flying flexible aircraft, which can regulate rigid-body motions, alleviate gust loads, reduce the wing root bendin...
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Keywords:
dynamic inversion;
nonlinear dynamic;
incremental nonlinear;
flexible aircraft ... See more keywords
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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j058692
Abstract: In this research, a loop-separation concept (LSC) is applied to a very flexible aircraft. Appealing features of this control architecture include decoupled control logic and the use of high-order m...
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Keywords:
control;
separation control;
loop separation;
flexible aircraft ... See more keywords