FIELD: electricity.
SUBSTANCE: invention relates to electrotechnical industry and can be used at manufacture of space vehicles (SV). A method for electrical checkouts of space vehicles consists in SV start and stop, including activation or deactivation of on-board electrical power sources or their ground simulators. An automated system supplies commands of control, access monitoring of discrete and analogue parameters as per data of the on-board telemetry and monitoring system of parameters of the on-board computation system, which are to be tracked. Besides, resistance of insulation of on-board buses relative to the frame and process signal parameters of the space vehicle are monitored. Directives of an automatic programme and an operator in a manual mode, as well as a test report and display of the current state of the test process is formed. Resistance of individual resistors is chosen based on geometrical progression.
EFFECT: improvement of reliability of an SV electrical checkout process.
2 cl, 1 dwg
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