Based on the quasi-six-degree-of-freedom flight dynamic equations, considering the changes in the elevation angle caused by an increase in the rolling angle during maneuvering turns, which leads to a rise in the radar cross-section. A computational model for the radar detection probability of ai...
Based on the quasi-six-degree-of-freedom flight dynamic equations, considering the changes in the elevation angle caused by an increase in the rolling angle during maneuvering turns, which leads to a rise in the radar cross-section. A computational model
For regression analysis, the equation can be written as Equations (3) and (4): Where A1and C are the model constants of tool materials, V is the sliding velocity in m/s, σnis the contact pressure in bars, T is the temperature in °C at the tool interface, and W is the tool wea...