Quadrotor Drone System Identification via Model-Based Design and In-Flight Sine Wave Injections

2020 ◽  
Author(s):  
Daniel S. Kaputa ◽  
Keith J. Owens
Author(s):  
Nopporn Patcharaprakiti ◽  
Jatturit Thongprong ◽  
Krissanapong Kirtikara ◽  
Jeerawan Saelao

2017 ◽  
Vol 7 (9) ◽  
pp. 911 ◽  
Author(s):  
Ying Ma ◽  
Haopeng Liu ◽  
Yunpeng Zhu ◽  
Fei Wang ◽  
Zhong Luo

2016 ◽  
Vol 26 ◽  
pp. 214-220 ◽  
Author(s):  
O. Adams ◽  
F. Klocke ◽  
M. Schwenzer ◽  
S. Stemmler ◽  
D. Abel

2012 ◽  
Vol 702 ◽  
pp. 26-58 ◽  
Author(s):  
Aurelien Hervé ◽  
Denis Sipp ◽  
Peter J. Schmid ◽  
Manuel Samuelides

AbstractControl of amplifier flows poses a great challenge, since the influence of environmental noise sources and measurement contamination is a crucial component in the design of models and the subsequent performance of the controller. A model-based approach that makes a priori assumptions on the noise characteristics often yields unsatisfactory results when the true noise environment is different from the assumed one. An alternative approach is proposed that consists of a data-based system-identification technique for modelling the flow; it avoids the model-based shortcomings by directly incorporating noise influences into an auto-regressive (ARMAX) design. This technique is applied to flow over a backward-facing step, a typical example of a noise-amplifier flow. Physical insight into the specifics of the flow is used to interpret and tailor the various terms of the auto-regressive model. The designed compensator shows an impressive performance as well as a remarkable robustness to increased noise levels and to off-design operating conditions. Owing to its reliance on only time-sequences of observable data, the proposed technique should be attractive in the design of control strategies directly from experimental data and should result in effective compensators that maintain performance in a realistic disturbance environment.


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