Calculation and Experimental Verification of Flush Air Data System Based on Kriging Model
摘要
Utilizing the Kriging model, a flush air data system has been devised specifically for a flying wing configuration vehicle. This system employs the surface pressure of the aircraft as its input, and outputs key atmospheric parameters, including velocity, angle of attack, and sideslip angle. The intricate mapping relationship between these inputs and outputs is precisely established through the application of the Kriging interpolation method. Experimental data from wind tunnel tests demonstrate the remarkable accuracy of the Kriging model when utilized for flush atmospheric data calculations.