Approach and landing of aircrafts with using signals of the satellite radionavigation systems

摘要

On the basis of the Markov theory of the random process optimal estimating the noise immunity suboptimal signal processing algorithms for on airborne integrated navigation and landing system (INLS) are synthesized. This INLS consists of the following components: an airborne combined GLONASS/GPS receiver, inertial navigation system, radio and barometric altimeters. Potential accuracy of the airborne INLS based on developed algorithms are analysed.