Velocity feedback control system for a rotor of a toy helicopter

• US 8,123,175 B2
• Filed: 12/24/2009
• Issued: 02/28/2012
• Est. Priority Date: 12/24/2009
• Status: Active Grant

• Current Assignee: Spin Master Limited (Spin Master Corp.)
• Original Assignee: Spin Master Limited (Spin Master Corp.)
• Inventors: Mak, Paul
• Primary Examiner(s): Michener, Joshua J
• Application Number:
  US12/647,129
• Publication Number:
  US 20110155842A1
• Time in Patent Office: 796 Days
• Field of Search: 244/17.11, 244/17.19, 244/17.21, 244/17.23, 244/17.13, 244/189, 244/190, 244/194, 73/66, 734/55, 734/60, 734/62, 734/64, 701/7, 701/8, 340/946, 340/967, 340/969, 340/974, 340/975, 700/729, 700/280, 700/63, 700/64, 700/69, 700/188, 356/27, 356/28, 356/285, 416/1, 416/25, 416/27, 416/30, 416/33, 416/35, 416/36, 416/43, 416/44, 416/47, 416/124, 416/126, 416/127, 416/128, 416/129, 416/130
• US Class Current: 244/194
• CPC Class Codes: G05D 1/0858 specially adapted for vertical take-off of aircraft

Abstract

There is provided a method and apparatus for controlling a toy helicopter in flight. The toy helicopter is powered by a first rotor and a second rotor. A target speed ratio is determined for the speed of the first rotor and the speed of the second rotor. The speed of the rotors is adjusted incrementally until the target ratio is achieved.

Claims

1. A method for controlling a helicopter, the helicopter having a first rotor and a second rotor, the method comprising the steps of:

(a) measuring a speed of the first rotor;

(b) determining a target second rotor speed based on the speed of the first rotor;

(c) measuring a speed of the second rotor;

(d) if the speed of the second rotor is greater than the target second rotor speed, decreasing power to the second rotor by a fixed increment;

(e) if the speed of the second rotor is less than the target second rotor speed, increasing power to the second rotor by a fixed increment;

(f) repeating steps (c), (d) and (e), until the speed of the second rotor and the target second rotor speed are within a predetermined margin,

wherein the first rotor is driven by a first motor, and the second rotor is driven by a second motor, and wherein power is provided to the first motor and the second motor using pulse width modulation (PWM),

wherein the step of measuring the speed of the first rotor comprises measuring the feedback voltage of the first motor, and

wherein the step of measuring the speed of the second rotor comprises measuring the feedback voltage of the second motor.

2. The method according to claim 1, wherein the second rotor is a tail rotor.

3. The method according to claim 1, wherein the second rotor is coaxial with the first rotor.

4. The method according to claim 1, wherein the step of determining the target second rotor speed depends on a trim position.

5. A method for controlling a toy helicopter, the helicopter having a rotor, the method comprising the steps of:

(a) reading a throttle position;

(b) determining a target rotor speed based on the throttle position;

(c) measuring a speed of the rotor;

(d) if the speed of the rotor is greater than the target rotor speed, decreasing power to the rotor by a fixed increment;

(e) if the speed of the rotor is less than the target rotor speed, increasing power to the rotor by a fixed increment;

(f) repeating steps (c), (d) and (e), until the speed of the rotor and the target rotor speed are within a predetermined margin,

wherein the rotor is driven by a motor, and wherein power is provided to the rotor using pulse width modulation (PWM), and

wherein the step of measuring the speed of the rotor comprises measuring the voltage a feedback voltage of the motor.

6. The method of claim 5, wherein the step of reading a throttle position comprises receiving a wireless command, wherein the wireless command specifies the throttle position.

7. A method of steering a toy helicopter, the helicopter having a first rotor and a second rotor, the method comprising the steps of:

(a) reading a steering position;

(b) measuring a first rotor speed;

(c) determining a target second rotor speed based on the first rotor speed and the steering position;

(d) measuring a second rotor speed;

(e) if the second rotor speed is greater than the target second rotor speed, decreasing power to the second rotor by a fixed increment;

(f) if the second rotor speed is less than the target second rotor speed, increasing power to the second rotor by a fixed increment;

(g) repeating steps (d), (e) and (f), until the second rotor speed and the target second rotor speed are within a predetermined margin,

wherein the first rotor is driven by a first motor, and the second rotor is driven by a second motor, and wherein power is provided to the first motor and the second motor using pulse width modulation (PWM),

wherein the step of measuring the speed of the first rotor comprises measuring the a feedback voltage of the first motor, and

wherein the step of measuring the speed of the second rotor comprises measuring the a feedback voltage of the second motor.

8. The method according to claim 7, wherein the step of determining the target second rotor speed comprises using a relationship associated with the steering position to compute the target second rotor speed from the first rotor speed.

9. The method according to claim 8 wherein the relationship is represented by a lookup table.

10. The method according to claim 8 wherein the relationship consists of multiplying the first rotor speed by a factor α

.

11. A toy helicopter comprising:

a first rotor powered by a first motor;

a second rotor powered by a second motor;

a power source configured to provide power to the first rotor and the second rotor using pulse width modulation (PWM); and

a microprocessor programmed with instructions for controlling the helicopter, the instructions comprising

(a) measuring a speed of the first rotor;

(b) determining a target second rotor speed based on the speed of the first rotor;

(c) measuring a speed of the second rotor;

(d) if the speed of the second rotor is greater than the target second rotor speed, decreasing power to the second rotor by a fixed increment;

(e) if the speed of the second rotor is less than the target second rotor speed, increasing power to the second rotor by a fixed increment;

(f) repeating steps (c), (d) and (e), until the speed of the second rotor and the target second rotor speed are within a predetermined margin,

wherein the first rotor is driven by a first motor, and the second rotor is driven by a second motor, and wherein power is provided to the first motor and the second motor using pulse width modulation (PWM),

wherein the step of measuring the speed of the first rotor comprises measuring the feedback voltage of the first motor, and

wherein the step of measuring the speed of the second rotor comprises measuring the feedback voltage of the second motor.

12. A toy helicopter comprising:

a first rotor powered by a first motor;

a second rotor powered by a second motor;

a power source configured to provide power to the first rotor and the second rotor using pulse width modulation (PWM); and

a microprocessor programmed with instructions for controlling the helicopter, the instructions comprising

(a) reading a throttle position;

(b) determining a target rotor speed based on the throttle position;

(c) measuring a speed of the rotor;

(d) if the speed of the rotor is greater than the target rotor speed, decreasing power to the rotor by a fixed increment;

(e) if the speed of the rotor is less than the target rotor speed, increasing power to the rotor by a fixed increment; and

(f) repeating steps (c), (d) and (e), until the speed of the rotor and the target rotor speed are within a predetermined margin,

wherein the rotor is driven by a motor, and wherein power is provided to the rotor using pulse width modulation (PWM),

wherein the step of measuring the speed of the rotor comprises measuring a speed of the first rotor or the second rotor;

wherein measuring the speed of the first rotor comprises measuring a feedback voltage of the first motor, and

wherein measuring the speed of the second rotor comprises measuring a feedback voltage of the second motor.

13. A toy helicopter comprising:

a first rotor powered by a first motor;

a second rotor powered by a second motor;

a power source configured to provide power to the first rotor and the second rotor;

using pulse width modulation (PWM); and

a microprocessor programmed with instructions for steering a toy helicopter, the instructions comprising

(a) reading a steering position;

(b) measuring a first rotor speed;

(c) determining a target second rotor speed based on the first rotor speed and the steering position;

(d) measuring a second rotor speed;

(e) if the second rotor speed is greater than the target second rotor speed, decreasing power to the second rotor by a fixed increment;

(f) if the second rotor speed is less than the target second rotor speed, increasing power to the second rotor by a fixed increment; and

(g) repeating steps (d), (e) and (f), until the second rotor speed and the target second rotor speed are within a predetermined margin,

wherein the first rotor is driven by a first motor, and the second rotor is driven by a second motor, and wherein power is provided to the first motor and the second motor using pulse width modulation (PWM),

wherein the step of measuring the speed of the first rotor comprises measuring a feedback voltage of the first motor,

wherein the step of measuring the speed of the second rotor comprises measuring a feedback voltage of the second motor.