Synthesis of angular stability loop on two–channel aircraft equipment in supersonic conditions
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https://doi.org/10.54939/1859-1043.j.mst.FEE.2023.29-34Keywords:
Angular stability loop; Fine-tuning filter; Solodovnikov method.Abstract
This paper presents a methodology for synthesizing the angular stability loop structure and determining the parameters of the fine-tuning filter on two–channel aircraft equipment in supersonic conditions. Based on distinctive parameters related to the geometry, mass, inertia, and aerodynamics of two–channel aircraft equipment in supersonic conditions, the authoring group conducted linearization and identified the structure of the angular stability loop. Subsequently, based on the Solodovnikov method, the parameters of the fine-tuning filter are determined according to predefined quality criteria. The simulation results, based on the constructed stability system, correspond to typical maneuvers of the target that affirm the accuracy of the proposed method.
References
[1]. Солодовников В.В.б Плотников В.Н., Яковлев А.В., “Теория автоматического управления техническими системами,” Изд-во МГТУ, 492с, (1993).
[2]. Пупков К.А., Егупов Н.Д., “Методы классической и современной теории автоматического управления: Том 3. Синтез регуляторов систем автоматического управления,” Издательство МГТУ им. Н.Э.Баумана, 616с, (2004).
[3]. Лебедев А.А., “Динамика систем управления беспилотными летательными аппаратами,” М., “Машиностроение”, 528с, (1965).
[4]. Лебедев А.А., Чернобровкин Л.С., “Динамика полета беспилотных летательных аппаратов,” М., “Машиностроение”, 616с, (1973).
