On Correcting the System of Inertial Navigation

摘要

Consideration is given to the simple algorithm of integration of inertial navigation system, satellite navigating system, magnetometer and the barometric sensor of altitude. A number of simplifying assumptions is introduced. This is due to the fact, that, on the one hand, the sensors in the considered system are not of high precision and, on the other hand, such systems are supposed to be used in objects moving with low velocity and on comparatively small distances. In particular, it could be cheap unmanned aerial vehicles. For illustration of opportunities of such system the example is considered.