A method for safe protection and return of UAV fuel quantity
A safety protection and unmanned aerial vehicle technology, which is applied in the field of automatic safety protection and return of the remaining fuel amount of the unmanned aerial vehicle, can solve the problems of hidden safety hazards, outstanding safety hazards of remaining fuel amount, and related alarms, etc., to reduce the possibility and improve the task Safety, flight time reduction effect
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[0039] Below in conjunction with specific embodiment the present invention is described in further detail:
[0040] The present invention comprises the following steps:
[0041] (1) The fitting curves of fuel consumption Fuel_Ex, throttle Thr_Eng and air pressure altitude H_Adc are obtained through the engine test, that is, when the UAV is in a certain air pressure altitude range, the fuel consumption and the throttle meet the following linear relationship: when x n ≤H_Adcn+1 , satisfy Fuel_Ex=K n ×Thr_Eng+b n , where n=1,2..., x is the specific value of the pressure altitude, K n is the fitting curve coefficient, b n is the offset;
[0042] (2) Before the UAV takes off, according to the actual loading of the UAV and the data collected by the barometric altimeter, the ground faces the flight control computer to bind the fitting curve obtained in step (1), the initial fuel quantity parameter Fuel_Ini and the initial height H_Ini; at the same time, set a remaining fuel quan...
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