Motor control method, apparatus, and system

Patent No. US10640224 (titled "Motor control method, apparatus, and system") on Aug 29, 2018. The application was issued on May 5, 2020.

What is this patent about?

’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.

How does this patent fit in bigger picture?

Technical Landscape

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.

Prosecution Position

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.

Claims

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.

Key Claim Terms New

Definitions of key terms used in the patent claims.

Term (Source)Support for SpecificationInterpretation
Compensation amount
(Claim 1, Claim 12)
The invention calculates a compensation amount of a control signal of the motor according to the present electrical parameter. This is used to modify the control signal. This adjustment ensures that even when battery voltage drops, the motor maintains the intended rotation speed requested by the flight controller.A calculated value used to adjust the motor's control signal to counteract the effects of declining battery voltage on motor rotation speed.
Control signal
(Claim 1, Claim 12)
The ESC receives a throttle signal sent from a flight controller. An increased high-level pulse width, i.e., an increased high-level pulse time duration, of the throttle signal may indicate that a higher rotation speed of the motor may be needed. The method modifies this control signal according to the compensation amount.The command sent to the motor or electronic speed controller (ESC), such as a throttle signal with a specific pulse width, that dictates the desired motor speed.
Present electrical parameter
(Claim 1, Claim 9, Claim 12)
The specification notes that a voltage of the battery continuously decreases during the discharging process. The method involves obtaining this parameter to address how the voltage outputted from the ESC to the motor decreases as the battery voltage decreases. This parameter allows the system to respond to the decreasing power of the unmanned aerial vehicle during a flight.A real-time measurement of the battery's state, specifically its voltage, used to detect fluctuations or decreases during the discharging process.
Voltage compensation amount
(Claim 9)
The method includes calculating a voltage compensation amount of the battery according to the present electrical parameter. It involves compensating an output voltage of the battery according to the voltage compensation amount to maintain the output voltage of the battery stable. This prevents the rotation speed of the motor from decreasing as the battery discharges.A specific adjustment value applied to the battery's output to ensure a consistent voltage level is supplied to the motor system despite battery depletion.

Litigation Cases New

US Latest litigation cases involving this patent.

Case NumberFiling DateTitle
1:23-cv-00055Jan 17, 2023Sz Dji Technology Co. Ltd. V. Textron Specialized Vehicles Inc.

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US10640224

Application Number
US16116279A
Filing Date
Aug 29, 2018
Publication Date
May 5, 2020
External Links
Slate, USPTO , Google Patents