Unmanned aerial vehicle gust load spectrum quick compiling method
A technology of load spectrum and wind gust, applied in design optimization/simulation, sustainable transportation, special data processing applications, etc., can solve the problems of large manpower and material resources, cumbersome process, etc.
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[0037] Taking a certain type of unmanned aerial vehicle as an example, the specific implementation steps of the method of the present invention are as follows:
[0038] 1) Calculate the reference eigenfrequency
[0039] Select a set of aircraft state parameters, including aircraft weight, height, Mach, wing average aerodynamic chord length, wing reference area, wing lift line slope, dynamic aerodynamic derivative, and use the two-degree-of-freedom rigid body analysis method that ignores the elastic mode to calculate Gust response characteristic frequency, these parameters and frequencies are used as "reference state parameters" and "reference characteristic frequency".
[0040] The four key benchmark state parameters are: M a = 0.3, 1 / μ g = 0.031, 1 / c = 0.808, 1 / A R =0.055, the reference characteristic frequency is: N 0 = 1.305.
[0041] 2) Construct a linear regression equation
[0042] Select 20 groups of aircraft state parameters, respectively use continuous turbulenc...
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