FIELD: procedure of indirect measurements of flight vehicle attitudes.
SUBSTANCE: the method is based on the use of information from the receiver of the satellite navigation system measuring the light vehicle velocity components to the South, East and in altitude from three-coordinate angular velocity and linear acceleration transducers installed on board the flight vehicle. The flight vehicle attitudes are measured in compliance with the estimation algorithm realized in the computer, on the varying time interval.
EFFECT: enhanced accuracy of measurement of the bank, pitch angle and the flight vehicle heading in the conditions of maneuvering.
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