A Method for Evaluating Energy Consumption of Effective Operation of Dynamic Load Electric UAV
An evaluation method and UAV technology, applied in the measurement of electrical variables, instruments, measuring devices, etc., can solve the problems of low air endurance, no correlation, and restrictions on the use of UAVs.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Publication Date
- 2019-08-13
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Abstract
Description
technical field
[0001] The invention relates to the field of energy consumption of unmanned aerial vehicles, in particular to a method for evaluating energy consumption of effective operations of electric-powered unmanned aerial vehicles with dynamic loads. Background technique
[0002] In recent years, the word "intelligence" has appeared more and more in people's lives. The emergence of agricultural plant protection drones is one of the distinctive features and symbols of agricultural intelligence. The agricultural spraying drone launched has a spraying efficiency 40-60 times that of manual work, and has a better effect on pest control. It completely liberates the labor and low efficiency of manual spraying. It is called an artifact of intelligent spraying. Life has become more colorful because of the development of technology, and agriculture has become more efficient because of technology. However, the two issues of battery life and more intelligent control are things ...
Examples
Embodiment Construction
[0042] The present invention will be further described below in conjunction with the examples and drawings, but the embodiments of the present invention are not limited thereto.
[0043] see figure 1 , the method for evaluating the energy consumption of the effective operation of the dynamic load electric powered unmanned aerial vehicle of the present embodiment includes the following steps:
[0044] Step 1. Measure and calibrate the unloaded mass M of the electric powered UAV 0 ;
[0045] Step 2. Install the variable-mass payload Z on the electric-powered UAV; the original mass of the payload is M, and the minimum mass is M k ;
[0046] Step 3: Start the operation of the electric-powered drone, maintain the motor speed and torque and control the weight of the load on the electric-powered drone to gradually decrease to M k , record the real-time motor voltage U, current I, battery output power P, remaining battery power SOC and flight distance S;
[0047]Step 4: Start the...