Method of test signal design for estimating the aircraft aerodynamic parameters
- 作者: Belokon’ S.A.1, Zolotukhin Y.N.1, Filippov M.N.1
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隶属关系:
- Institute of Automation and Electrometry, Siberian Branch
- 期: 卷 53, 编号 4 (2017)
- 页面: 358-363
- 栏目: Automation Systems in Scientific Research and Industry
- URL: https://journals.rcsi.science/8756-6990/article/view/212182
- DOI: https://doi.org/10.3103/S8756699017040070
- ID: 212182
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详细
A method of test signal design is proposed for studying the aircraft aerodynamic characteristics with the use of the technology of dynamically scaled free-flight models. Simultaneous excitation of all input channels in a prescribed frequency band by a set of mutually orthogonal signals is applied to increase the efficiency. A modified method of calculating the set of mutually orthogonal sinusoidal signals with a small normalized peak factor is presented. Results of simulating the aircraft motion in the MATLAB/Simulink environment with the use of the developed method of test signal design are reported.
作者简介
S. Belokon’
Institute of Automation and Electrometry, Siberian Branch
编辑信件的主要联系方式.
Email: serge@idisys.iae.nsk.su
俄罗斯联邦, pr. Akademika Koptyuga 1, Novosibirsk, 630090
Yu. Zolotukhin
Institute of Automation and Electrometry, Siberian Branch
Email: serge@idisys.iae.nsk.su
俄罗斯联邦, pr. Akademika Koptyuga 1, Novosibirsk, 630090
M. Filippov
Institute of Automation and Electrometry, Siberian Branch
Email: serge@idisys.iae.nsk.su
俄罗斯联邦, pr. Akademika Koptyuga 1, Novosibirsk, 630090
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