Automatic amplitude modulation frequency scanning method for airplane servo elasticity frequency response test
A technology of servo elasticity and aircraft, applied in the direction of adaptive control, electrical test/monitoring, control/adjustment system, etc., can solve the problems of large error of test data, inability to guarantee the safety of rudder surface structure and signal-to-noise ratio of loop response signal at the same time
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[0060] 1. Acceleration sensors are arranged on the trailing edge of the aircraft control surface;
[0061] 2. Reference Figure 4 Disconnect the feedback loop of the flight control system of the aircraft between the output end of the rudder deviation command of the flight control computer and the synthesis end of the forward command of the actuator, and connect it to the real-time simulation system;
[0062] 3. Build an automatic AM sweep simulation model in the real-time simulation system. The automatic AM sweep simulation model includes a constant-amplitude step sine excitation signal generation function module, an automatic AM signal generation function module, and a loop dynamic characteristic calculation function module;
[0063] 4. Refer to Figure 4 , according to the text description in the figure, complete the signal transmission connection between the equal-amplitude step sine excitation signal generation module, the automatic amplitude modulation signal generation ...
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