Calibration algorithm development for inertial navigation system with use of two-axis motion simulator
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractCalibration method and algorithm for high-accuracy inertial navigation system are considered. As an input to the calibration algorithm uses the signals from the output of the system (coordinates, velocity and orientation angles). The method and algorithm which is given in article are realized on two-axis motion simulator.An example of work of inertial system calibration simulation software is given.
Keywords:calibration; motion simulators; gyroscope;accelerometer; algorithm; inertial navigation system