ALGORITHM OF INS CORRECTION ON THE BASE OF RANGE INFORMATION

N.P. Rybak, I.V. Seden

Анотація


 Inertial navigation system is a universal navigation system for determination of trajectory motions and angular coordinates (roll, pitch, and heading angles) of aircraft. Unlimited increasing of errors in time is essential disadvantage of INS, so the methods of correction of these systems have a great importance.

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Посилання

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