FIELD: measuring technology.
SUBSTANCE: invention is related to devices for monitoring and measuring the parameters of systems that are part of the sighting and navigation flight system of an aircraft. The control and verification complex of systems of sighting and navigation flight complex of the aircraft contains an industrial computer with software for controlling the components of the complex, as well as processing and storing data obtained as a result of verification, an interface converter, a measuring unit, a monitoring and control unit, a control and measurement unit, a switching and control unit, consisting of a switching unit, a measurement unit, a voltage driver and a transformer, an uninterruptible power supply and power supplies. At the same time, the industrial computer with software is connected to an interface converter, which is connected via input-outputs to the measuring unit, the monitoring and control unit, the control and measurement unit, and the switching and control unit, and the switching unit is connected via inputs to a voltage driver and a transformer, and its outputs are connected to the measurement unit, the control and measurement unit, the monitoring and control unit and the measuring unit. The uninterruptible power supply is connected via its outputs to the industrial computer, the switching and control unit, as well as the measuring unit, the power sources are connected via their outputs to the input of the switching unit and the input of the transformer, via by their input-output to the interface converter. The control and verification complex is configured to connect the object of control through the inputs and outputs of the measuring unit, the monitoring and control unit, the control and measurement unit and the switching and control unit.
EFFECT: expanding the functionality of the control and verification complex for testing the systems of the sighting and navigation flight complex of the aircraft.
1 cl, 1 dwg
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Authors
Dates
2023-07-04—Published
2022-06-06—Filed