ALGORITHM OF INS CORRECTION ON THE BASE OF RANGE INFORMATION
Автор(и)
N.P. Rybak
National Aviation University, Kyiv
I.V. Seden
National Aviation University, Kyiv
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.
