Aircraft path tracking method based on variable forward distance LOS guidance law
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[0076] Taking the path tracking problem in the horizontal plane of a typical surface-symmetric cruise vehicle as an example, the schematic diagram is as follows figure 1 Shown in a: The component L of the lift force in the plumb direction during the banked turn of the aircraft 1 Balanced with gravity G=mg, the horizontal component of lift L 2 It is used to provide the lateral overload required for the aircraft to turn. The cruising flight speed V of the aircraft is 100m / s, the initial position is (0,0) (unit: m), the initial heading is along the direction of true north (ψ=0°), and the desired path is composed of waypoints A(0,1000) and B(1000,3000) is determined (unit: m). The parameter design related to the path tracking system is shown in the following table:
[0077] Table 1. Path tracking system related parameters
[0078]
[0079] The aircraft path tracking method based on the variable forward distance LOS guidance law proposed by the present invention first determ...
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