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Stability Control System for a Propeller Powered by a Brushless DC Motor Codey Lozier & Christian Thompson Advisor Dr. Mohammad Saadeh
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Control Systems Applications Cruise control Automation in factories
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Stability Control System Design a control system that stabilizes a horizontal beam
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Project Deliverables Research all components needed to design the control system Understand how the signals of each component are transmitted and read Gain knowledge of LabVIEW driven environment Design a functioning prototype using components Gain knowledge of control systems Implement a control system that uses a PID controller Research paper
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Background: Electrical Components Primary Components Control System Brushless DC motor Electronic Speed Controller Carbon fiber propeller Microcontroller Rotary Encoder Data Acquisition Device Secondary Components Testing Wheatstone Bridge board Micro load cell Encoder Data Acquisition Device
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Brushless DC Motor (BLDC) High performance motor 27,000 – 30,000 RPM Brushless characteristics Permanent magnet Electrically commutated Driven using PWM Ideal for long term applications
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Lift Force Of the four forces of flight, we are only concerned with two: Lift Force & Weight Force Opposing forces The airfoil of an airplane’s wing is just like a propeller blade
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Schematic of Air Flow X Y
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Pressure Variation Along Slipstream P 2 P 4 = P 1 = P atm
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Lift Force (cont.) Movement of air Forces above and under the blade
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Modifications to BLDC Original propeller could not generate enough lift force Replaced with 8 x 4.5 carbon fiber (10g) propeller
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Brushless Speed Controller Electronic speed controller (ESC) Powers motor (17Vdc) Used in high power RC systems Receives PWM signals from Arduino Mega
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Arduino Uno Microcontroller Board Based on the Atmega 328P Microcontroller Ideal for prototyping Open source Resources Pulse Width Modulation Commutation
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YUMO Rotary Encoder Sensor Position Speed Direction High resolution Resources Interfaced with DAQ device
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Multifunction Data Acquisition Device Plug and Play Programmed using LabVIEW All components are interfaced with this device
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Secondary Components & Testing Secondary components Micro load cell Wheatstone Bridge Encoder DAQ device Testing Setup of components Signal Processing
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Micro Load Cell Force sensing element Strain gauges Change in electrical resistance
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Phidget Bridge: Wheatstone Contains 4 Wheatstone Bridges USB interface ( 2 ) Amplifies signal sent from micro load cell ( 1 ) Demo applications are provided Users can develop own applications
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Micro Load Cell Calibration Calculate lift force Methods used for calibration Demo Program Labview Instrumentation Amplifier
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Calculating Lift Force Several Trials Flipped propeller Data exported to Excel Used to develop lift force equation
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Encoder Data Acquisition Device Interfaced with rotary encoder Includes demo application Libraries LabVIEW C/C++ Calculate RPM of BLDC
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Rotary Encoder Setup Shaft is stabilized with pillow block Device is fixed to table Interfaced with data acquisition device
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Brushless DC Motor Setup
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Experimental Setup
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LabVIEW System design platform and development environment Graphical programming language Virtual Instrument (VIs) Applications Data Acquisition Instrument Control Automation Control System Design
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LabVIEW Interface
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Current Progress Spring 2014 Researched and acquired all components of project components of experimental prototype electrical components pros and cons understand how to transmit and read signals Designed an experimental prototype of system Integrated components into experimental system
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Current Progress Summer 2014 Gained understanding of LabVIEW driven environment Designed applications for all components Incorporated a Multifunction I/O Data Acquisition Device using LabVIEW Developed VIs for all components Integrated all components
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Future Progression October 2014 Develop a control system using LabVIEW Incorporate a PID controller into control system November 2014 Add a second BLDC motor on opposite end of beam Modify control system using the second motor Research Paper
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