Control method of aseismic airbag of fixed-wing unmanned target aerial vehicle
A technology of shock-absorbing airbags and control methods, applied in pump control, aircraft parts, mechanical equipment, etc., can solve problems such as damage to target drones, inability to meet shock-absorbing needs, and achieve the effect of meeting shock-absorbing needs
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[0027] Below in conjunction with accompanying drawing, the implementation of the present invention will be further described:
[0028] The invention relates to a method for controlling a shock-absorbing airbag of a fixed-wing unmanned target drone. Specifically, it includes the following steps:
[0029] 1) After the fixed-wing unmanned target drone receives the landing signal, the unmanned target drone collects the parameter information at this time;
[0030] 2) Process the collected information and calculate the optimal internal pressure value of the shock-absorbing airbag;
[0031] 3) Collect the actual pressure inside the shock-absorbing airbag, and operate the inflatable fan to make the shock-absorbing airbag reach the optimal internal pressure;
[0032] 4) When the fixed-wing unmanned target drone lands, stop the fan.
[0033] The parameter information includes the height, temperature, fuel consumption, speed and acceleration of the fixed-wing unmanned target drone.
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