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ES 100 Micro Air Vehicle Project. Montgomery College Professor: Dr. Charles Kung Summer I 2012. Team Members: Andrew Joe Laura Mohammad Nathelie Noella Stephanie Thomas. Introduction.
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ES 100 Micro Air Vehicle Project Montgomery College Professor: Dr. Charles Kung Summer I 2012 Team Members: Andrew Joe Laura Mohammad Nathelie Noella Stephanie Thomas
Introduction Our goal is to design a Unmanned Aerial Vehicle (UAV) that can successfully complete the field test equipped with a surveillance mechanism that it can use to capture footage and video.
Objectives The UAV must pass a field test and the requirements include: • UAV must be able to take off and land from tennis court • Flight test should be at least 2 minutes long • UAV must capture video footage from flight to landing
Constraints The UAV must: • Have an operator that uses great caution to ensure the safety/security of any onlookers • Safe/operable design • Weigh a maximum of 450 grams • Operate by battery power (Lipo 1000 mAh, 11.1V , 20C Battery ) • Use a suitable RC frequency (2.4 Ghz)
Plan of Action Steps to completing the project: • Elect a group leader and assign roles • Brainstorm designs that meet with the objectives and constraints • Cost comparison and analysis • Trainer flying practice • Preliminary design process • Design comparison and analysis • Assembly of aircraft • Practice flying the aircraft • Final flight test and evaluation
Description Things we want to accomplish: • Build a UAV with a camera mount attachment • Minimize cost expenses • Maintain performance and reliability • Maximize and determine the most suitable components
Type of UAV Design Fixed Wing Design
Navigational System Remote Control
Propulsion System Propeller Propulsion
Take-off Mechanism Accelerated Take-off on the surface of Tennis Court
Tail Design Simple Tail Design with a Rudder, Elevator, and Horizontal/Vertical Stabilizer
Camera Mount Design Our Designed Camera Mount
Mechanisms for Securing Components Screws/Bolts and Double Sided Tape
Flight Trainer Chosen The Night Vapor RTF
Basic Platform Chosen The GWS Slowstick Airplane ARF
Motor, Servos, and Power System Chosen Dynamic Power System Kit
Battery and Charger Chosen Sky Lipo Battery and Charger Kit (1000 mAh, 11.1 V, 20 C)
Design Details Battery Mount Camera Mount
Vertical Stabilizer Horizontal Stabilizer
Elevator Fuselage
Leading Edge Wing Support Trailing Edge Wing Support
Motor Motor Mount
Propeller Rudder
Tail Gear Support Servo Tray
Wheel Wing
Things to Consider for Assembly • Center of Gravity • Securing the Components
Problems We Experienced • Lack of Flight Experience • Unfinished Aircraft Assembly • Unavailable Battery
List of Materials • 1 Slow Stick Airplane ARF: No Power Supply • 1 3 pc Dynamics Brushless Motor +18A with 9g Servos • 1 Sky Lipo 1000 mAh, 11.1V , 20C Battery
References • Aviation Knowledge - http://aviationknowledge.wikidot.com/aviation:parts-airplane • Google Images - http://www.google.com/images • Google maps - http://www.maps.google.com/ • Sample Project Report - http://www.montgomerycollege.edu/sample_mav_report.pdf • RCSgroups - http://www.rcgroups.com/forums/showthread.php?t=917604 • Frequency Picture - http://rrsg.ee.uct.ac.za/members/jwamicha/usrp2_fft-SignalGenerator-Off.png