FULL TEXT IN RUSSIAN
Mekhatronika, Avtomatizatsiya, Upravlenie, 2018, vol. 19, no. 2, pp. 134—138
DOI: 10.17587/mau.19.134-138
Account of Errors of Transducer during Inspection of Flying Device
G. P. Shibanov, gpshibanov@mail.ru, Government Test-flight Center named after V. P. Chkalov, Akhtubinsk, Russian Federation
Corresponding author: Shibanov Georgy P., D. Sc., Professor, Leading Researcher, Government Test-flight Center named after V. P. Chkalov, Akhtubinsk, Russian Federation, e-mail: gpshibanov@mail.ru
Accepted on November 02, 2016
Any structure of automation means of checkout flight parameters of flying device and diagnostics of onboard equipment which taking as a basis on linearization mathematical model of flying device will have another description for non-linearity mathematical model this flying device. In this case automation means of checkout employment practice unfit for testing of parameters of flight and diagnostics of onboard equipment. Estimation effectiveness of automation diagnostics of onboard equipment and checkout parameters of flight require employment of new methods and approach independently from the dynamics of flying device and adequate of mathematical models everybody of checkout process. Indignation of atmosphere and instrumental errors of transducers exercise influence on selection of scheme checkout and diagnostics. They can be determine of dynamics systems of checkout and diagnostics. At the same time sensor errors or errors of transducer can be detect and become localized without use altogether vector of estimation condition of checkout and diagnostics object. It can be make by means of weigh-procedure of measuring estimation error and off-error exit each of measuring canal. This article consideration the algorithms account of instrumental errors of transducers during inspection of flying device.
Keywords: account, error, transducer, checkout, diagnostics, measuring channel, estimation vector, flying device
For citation:
Shibanov G. P. Account of Errors of Transducer during Inspection of Flying Device, Mekhatronika, Avtomatizatsiya, Upravlenie, 2018, vol. 19, no. 2, pp. 134—138.
DOI: 10.17587/mau.19.134-138
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