The equation is used to find the total current in the parallel circuit and series circuit on the quadcopter drone component, then a drone flight test is carried out for data collection and continued with data analysis. The research was carried out starting with the assembly of a quadcopter drone, each component would then calculate the total current. In addition, the calculation uses parameters in the form of current from the components on the quadcopter board which is added to the current in the brushless motor which is converted from PWM (Pulse Width Modulation). This study describes the design of the quadcopter control system and focuses on the analysis of calculating battery capacity, power consumption calculated from distance and flight time. Energy consumption is an important constraint for drone flight operations to reach their full potential in performing flights of optimal duration and range. ![]() ![]() The power source in quadcopter drones is generally a lithium battery with a flight duration that depends on the load, distance, speed of the drone. Quadcopter development currently focuses a lot on autopilot features that allow drones to fly autonomously. Quadcopter is one of the Unmanned Aerial Vehicles that can fly vertically.
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