Hardware and software complex for tests power supply and control systems electric plasma propulsion
Автор: Chubov S.V., Mikhaylov M.V., Soldatov A.I.
Рубрика: Системы навигации и управления авиационно-космической техники
Статья в выпуске: 4 т.17, 2017 года.
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This article provides a variant of constructing a hardware-software system for testing the power supply and control system of electric-plasma propulsion based on electronic controlled loads, power supplies and the LTR-EU-16-2 measuring crate system of the company “L Card”, which has a modular architecture of 16 seats, allowing you to re-complete the system with other modules or expand the configuration. The software is based on a system-independent client-server management interface. The proposed solution for using an automatic complex with standard electronic loads and data collection tools based on the LTR41, LTR11, LTR210 modules with galvanic isolation is preferable, because it will allow to achieve high accuracy and speed of measurement, will significantly reduce the costs and time for the production of verification equipment, and also Will improve the quality of testing with different types of power supply and control systems.
Power processing unit, hardware and software complex, stationary plasma thruster
Короткий адрес: https://sciup.org/147155217
IDR: 147155217 | DOI: 10.14529/ctcr170414