SYSTEM FOR CORRECTION OF INACCURACIES OF INERTIAL NAVIGATION SYSTEMS
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United States of America Patent
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Issued Date -
Jul 7, 2011
app pub date -
Dec 30, 2010
filing date -
Jan 7, 2010
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
The system is formed by the first differential pressure sensor where its one input is connected by means of the first pressure feed to the first monitoring point of the body and where its second input is connected by means of the second pressure feed to the second monitoring point. Output of the first differential pressure sensor is connected via amplifying element to the input of analogue-digital converter and its output is connected to the microprocessor system. This is formed by mutually interconnected blocks, specifically the block with inputs, processing unit, memory and the block with output circuits, and together with the whole measuring system it is connected to the block of power supply distribution, which is interconnected with external power supply source. The first output of the microprocessor system is connected to display device. The first monitoring point and the second monitoring point are located symmetrically in relation to the centre of gravity of the body. Microprocessor system is equipped with the second output used to control external devices.
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