Abstract:Aiming at the problem that the flush air data sensor system (FADS) and inertial navigation system (INS) are prone to inaccurate parameter estimation caused by wind speed changes when calculating aircraft air data. An air data solution method is proposed in this paper to integrate FADS/INS/meteorological observation data. The FADS calculates the air data based on the pressure distribution on the outer surface of the aircraft directly. The INS provides the attitude angle and acceleration. Meteorological observation data include the pressure altitude correspondence and wind speed vector. The fusion process combines the FADS pressure model, aircraft motion model and air data to build the state and observation equation, and uses filtering preprocessing and extended Kalman filter to estimate the precise airspeed vector and altitude, and further converts the INS data to obtain the air data. Simulation results show that the method proposed in the paper is effective in improving the estimation accuracy by reducing the estimation error by 30% in angle of attack and sideslip estimation, 89% in Mach estimation, and 93% in barometric altitude compared with the existing algorithms without fused meteorological observation data.