Stability Control System for a Propeller Powered by a Brushless DC Motor Codey Lozier & Christian Thompson Advisor Dr. Mohammad Saadeh
Control Systems Applications Cruise control Automation in factories
Stability Control System Design a control system that stabilizes a horizontal beam
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
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
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
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
Schematic of Air Flow X Y
Pressure Variation Along Slipstream P 2 P 4 = P 1 = P atm
Lift Force (cont.) Movement of air Forces above and under the blade
Modifications to BLDC Original propeller could not generate enough lift force Replaced with 8 x 4.5 carbon fiber (10g) propeller
Brushless Speed Controller Electronic speed controller (ESC) Powers motor (17Vdc) Used in high power RC systems Receives PWM signals from Arduino Mega
Arduino Uno Microcontroller Board Based on the Atmega 328P Microcontroller Ideal for prototyping Open source Resources Pulse Width Modulation Commutation
YUMO Rotary Encoder Sensor Position Speed Direction High resolution Resources Interfaced with DAQ device
Multifunction Data Acquisition Device Plug and Play Programmed using LabVIEW All components are interfaced with this device
Secondary Components & Testing Secondary components Micro load cell Wheatstone Bridge Encoder DAQ device Testing Setup of components Signal Processing
Micro Load Cell Force sensing element Strain gauges Change in electrical resistance
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
Micro Load Cell Calibration Calculate lift force Methods used for calibration Demo Program Labview Instrumentation Amplifier
Calculating Lift Force Several Trials Flipped propeller Data exported to Excel Used to develop lift force equation
Encoder Data Acquisition Device Interfaced with rotary encoder Includes demo application Libraries LabVIEW C/C++ Calculate RPM of BLDC
Rotary Encoder Setup Shaft is stabilized with pillow block Device is fixed to table Interfaced with data acquisition device
Brushless DC Motor Setup
Experimental Setup
LabVIEW System design platform and development environment Graphical programming language Virtual Instrument (VIs) Applications Data Acquisition Instrument Control Automation Control System Design
LabVIEW Interface
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
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
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