The features of an aircraft landing approach on a moving aircraft carrier are studied. The main measuring systems used in landing approach for a carrier-based aircraft are inertial and satellite navigation systems. Joint signals processing in the navigation system is carried out by using an adaptive Kalman filter that can operate in the absence of a priori information about the statistical characteristics of the input noise. Kalman adaptive filter is based on using the properties of the updated sequence. The simulation results according to the semi-natural experiment showed its high efficiency.