SYSTEM AND METHOD FOR DETERMINING SPATIAL POSITION AND HEADING OF AIRBORNE VEHICLE Russian patent published in 2014 - IPC G01C23/00 

Abstract RU 2505786 C2

FIELD: instrument making.

SUBSTANCE: temperature sensors are introduced to a unit of angular velocity sensors, a unit of linear acceleration sensors and a three-component magnetometer. The latter is connected through an analogue-to-digital converter to a calculator. In-series connected switching assembly, buffer stage, interface module and interface assembly are connected to the calculator. Calibration characteristics of the unit of angular velocity sensors, the unit of linear acceleration sensors and the magnetometer are used considering ambient air temperature variation.

EFFECT: improving reliability and accuracy of the system.

3 cl, 1 dwg

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RU 2 505 786 C2

Authors

Semenov Igor' Alekseevich

Samojlov Viktor Mikhajlovich

Dates

2014-01-27Published

2012-04-17Filed