Patent No. US10640224 (titled "Motor control method, apparatus, and system") on Aug 29, 2018. The application was issued on May 5, 2020.
’224 is related to the field of unmanned aerial vehicle (UAV) propulsion systems and, more specifically, to the management of motor performance as a power source depletes. In typical drone applications, an electronic speed controller (ESC) regulates motor speed based on throttle signals from a flight controller; however, as the battery voltage naturally drops during discharge, the motor’s rotational speed and responsiveness diminish even if the throttle input remains constant. This leads to reduced mobility and sluggish flight characteristics as the battery drains.
The underlying idea behind ’224 is to decouple motor performance from the fluctuating state of the battery by implementing a dynamic adjustment layer between the flight controller and the motor. Instead of allowing the motor to receive a raw, diminishing voltage, the system treats the battery’s state as a variable that must be neutralized. By monitoring real-time electrical changes, the system can apply a calculated offset to the control logic or the power delivery itself, ensuring that a specific throttle command results in the same thrust output regardless of whether the battery is at 100% or 20% charge.
The claims of ’224 focus on a method and apparatus that obtain a present electrical parameter of the battery—such as voltage, current, or internal resistance—and use this data to calculate a compensation amount. This compensation is then applied to the motor's control signal or used to stabilize the battery's output voltage directly. The independent claims specifically cover the closed-loop process of sensing the battery's state, determining the necessary correction factor, and modifying the motor's operational signal to maintain consistent performance.
In practice, the invention functions by utilizing a feedforward or feedback control loop that adjusts the pulse width of the throttle signal or the voltage levels sent to the motor. For example, if the system detects a voltage drop, it can increase the high-level pulse duration of a rectangular wave signal to effectively 'boost' the motor back to its intended RPM. Alternatively, the system can use a hardware-based approach where an external power supply is switched in to compensate for the voltage loss, maintaining a stable bus voltage for the ESC.
This approach differs from prior solutions that relied on the pilot or flight controller to manually increase throttle to account for battery sag. By integrating real-time voltage modeling and automated signal modification, the invention ensures that the UAV's flight dynamics remain predictable throughout the entire discharge cycle. This eliminates the 'slow response' issues common in high-mobility maneuvers, providing a consistent power profile that allows the flight controller to operate with higher precision and reliability.
In the mid-2010s when ’224 was filed, unmanned aerial vehicle propulsion systems were typically implemented using a direct electrical coupling between a battery source and an electronic speed controller. At a time when motor speed was commonly regulated by mapping pulse-width modulated throttle signals directly to output voltages, systems relied on the assumption of a relatively stable power source to maintain consistent thrust characteristics. However, hardware constraints related to the chemical discharge curves of lithium-based batteries made maintaining uniform motor performance non-trivial, as the gradual depletion of the power source resulted in a corresponding decay of the maximum achievable voltage and rotational velocity for any given control input.
The disclosed invention achieves a technical advancement in flight stability and responsiveness by introducing a dynamic compensation layer between the power source and the motor control logic. By integrating real-time monitoring of battery electrical parameters—such as voltage or internal resistance—the system calculates a specific compensation amount to modify the motor control signal or the output voltage itself. This architectural shift allows the propulsion system to decouple motor performance from the state-of-charge of the battery, overcoming the technical constraint of power decay during flight. The resulting capability enables consistent mobility and thrust response throughout the entire discharge cycle, ensuring that a specific throttle command yields a predictable mechanical output regardless of the remaining battery capacity.
This patent contains a total of 17 claims, with claims 1, 9, and 12 serving as the independent claims. The independent claims focus on methods and an apparatus for motor control that involve obtaining real-time electrical parameters from a battery, such as voltage or charge levels, to calculate and apply compensation amounts to control signals or output voltages to ensure operational stability. The dependent claims serve to further define the specific types of electrical parameters monitored, detail the mathematical models and timing used for calculating compensation, and specify the hardware components, such as detection circuits and processors, required to implement the control system.
Definitions of key terms used in the patent claims.
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