Method for determining airplane critical circumvention parameters in low-altitude wind shear
A low-altitude wind shear and method-determining technology, which is applied in electrical digital data processing, special data processing applications, instruments, etc., can solve problems such as long working hours, heavy workload, and low efficiency
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[0054] It is known that the detection distance of the aircraft is L=[500,1000]m; the wind shear scale is 2000m. Firstly, the avoidance turning radius R of the aircraft is calculated according to the formula in calculation step 1. The calculation results are as follows:
[0055] Table 1 Avoidance turning radius R
[0056]
[0057] Substitute the calculated evasive turning radius R into the calculation formula in step 2, and calculate the normal overload coefficient n at different speeds z , as shown in Table 2.
[0058] Table 2 Normal overload factor n z
[0059]
[0060] The normal overload factor n z Substituting the formula in step 3 to get the turning time t of the aircraft, the calculation results are shown in Table 3:
[0061] Table 3 Aircraft turning time t
[0062]
[0063] The normal overload factor n z Substituting the formula in step 4, the aircraft turning angular velocity ω and aircraft slope φ at different speeds can be calculated. The calculation res...
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