Charging method based on aerial drone charging station device
A charging method and technology of drones, which are applied in the field of drones, can solve problems such as power exhaustion of drones, waste of resources, and unfavorable operations.
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Embodiment 2
[0056] Embodiment 2 includes all the structures and steps of Embodiment 1. In Embodiment 2, the second controller combines the GPS locator to measure the remaining flight route of the drone, and obtains the remaining flight distance. The remaining flight distance is less than the set threshold , select the normal charging mode, and the second controller turns on the switch K to charge the UAV normally.
Embodiment 3
[0057] Embodiment 3 includes all the structures and steps of Embodiment 1, and Embodiment 3 also includes the fault detection process of the pressure sensor:
[0058] The initial value of j is set to 1 in the first controller, the initial value of i is 1, and a fault threshold E is set;
[0059] The first controller calculates the local maximum value of the current signal u(t) of the pressure sensor and obtains the upper envelope u through cubic spline interpolation up (t);
[0060] Calculate the local minimum of the signal u(t) and obtain the lower envelope u by cubic spline interpolation low (t);
[0061] Define the mean envelope m 1 (t)=[u up (t)+u low (t)] / 2;
[0062] Using the formula h j (t)=u(t)-m j (t) Calculate the difference h j (t);
[0063] if h j (t) does not meet the IMF screening stop condition, make u(t)=h j (t), the value of j is increased by 1, and the return pair h j (t) continue to decompose; when h j (t) Satisfies the IMF screening stop condi...
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