Abstract
The purpose of this article is to develop an algorithm for setting the speed of air pressure change used in control systems of air-speed flight parameters (CSASFP) of aircrafts, and to assess setting speed accuracy. Research methods include theories of automatic control and system modeling, as well as the basic laws and provisions of gas dynamics. Results of studies of the processes of airflow with constant pressure drops through the throttling sections of CSASFP were used to develop a mathematical model of a pressure regulator that implements an algorithm for setting the pressure change speed, the main parameters of gas-dynamic processes occurring in a closed volume in which the pressure change speed is set are established. Dependencies are established to assess the accuracy of setting air pressure change speed. Experimental studies of the process of setting the air pressure change speed in a closed volume were carried out, which confirmed the accuracy of the proposed algorithm. The algorithm for setting air pressure change speed in a closed volume is calculated and can be used to solve problems of designing CSASFP in which modern control methods can be implemented.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Markov AV (2014) Problems and ways of absolute pressure sensors quality control systems modernization. Age Qual 4:30–32
Markov AV (2015) Concept of measuring instruments of absolute pressure sensors quality control systems. Age Qual 1:34–35
Markov AV (2018a) Mathematical model of automated deadweight absolute pressure control system. Vestnik IrGTU 22(11):112–125
Pushkov SG, Lovitsky LL, Korsun ON (2018) Aero-dynamic errors of the aircraft static pressure measurement systems in sliding modes. Meas Tech 2:37–42
Pushkov SG, Gorshkova OYu, Korsun ON (2013) Mathematic models of in-flight measurements of speed and angle of attack in aircraft landing modes. Mech Autom Control 18:66–70
Korsun ON, Nikolaev SV, Pushkov SG (2016) Algorithm for estimating systematic errors in airspeed measurements, angles of attack and slip in flight tests. In: Proceedings of the Russian Academy of Sciences. The theory of control systems, vol 3, pp 118–12
Markov AV (2018) The concept of precision automated control systems for pressure sensors as a means of metrological support of aircrafts. In: Questions of defense technology. Series 16: Technical means of countering terrorism 9–10(123–124), pp 150–154
Markov AV (2018b) The concept of precision automated deadweight piston quality control systems for pressure sensors quality. Innov Educ 4:89–93
Mirskaya VA, Nazarevich DA, Ibavov NV (2017) Method of pressure measurement on an experimental installation for studying the complex of thermophysical properties of liquids and gases. Meas Tech 9:33–36
Mirskaya VA, Ibavov NV, Nazarevich DA (2016) Automated experimental installation for investigating the complex of thermophysical properties of liquids and gases. Thermophys Temp 54(2):237–242
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2021 The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerland AG
About this paper
Cite this paper
Markov, A. (2021). Accuracy Assessment of Setting Pressure Change Speed in Aircraft Control Systems of Air-Speed Flight Parameters. In: Radionov, A.A., Gasiyarov, V.R. (eds) Proceedings of the 6th International Conference on Industrial Engineering (ICIE 2020). ICIE 2021. Lecture Notes in Mechanical Engineering. Springer, Cham. https://doi.org/10.1007/978-3-030-54817-9_135
Download citation
DOI: https://doi.org/10.1007/978-3-030-54817-9_135
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-54816-2
Online ISBN: 978-3-030-54817-9
eBook Packages: EngineeringEngineering (R0)