Answers are grounded in this paper and cite their sources.
Differential error equations are derived for the navigation errors of a local level undamped pure inertial platform that continuously rotates in azimuth. From these, the time response equations for the vector position error produced by a constant level gyro drift error, as a function of platform rotation rate, are computed and evaluated. It is shown that platform rotation attenuates the system position error due to level gyro bias and that this attenuation is a nonlinear function of rotation rate.
No takes yet. Share an insight, caveat, or question.
Edward S. Geller (1968) studied this question.
Synapse has enriched 10 related papers. Consider them for comparative context: