FIELD: instrumentation.
SUBSTANCE: invention relates to the field of instrumentation and can be used in strapdown inertial navigation systems, in particular strapdown orientation systems. The substance of the claimed invention lies in the fact that the first module of the satellite navigation system is introduced into the device, connected to the input of the microcontroller, located inside the housing. At the same time, at least one first external antenna is connected to the first module of the satellite navigation system, the second module of the satellite navigation system is also introduced into it, connected to the input of the microcontroller, located inside the housing. At the same time, at least one second external antenna is connected to the second module of the satellite navigation system.
EFFECT: increasing the accuracy of determining the angles of spatial orientation of dynamic and static objects, as well as ensuring the determination of the angles of spatial orientation only according to the indications of satellite navigation systems in the event of failure of inertial sensors.
3 cl, 1 dwg
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Authors
Dates
2023-05-02—Published
2022-04-11—Filed