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P09123 – 2009 RIT MAV Platform Project Review

P09123 – 2009 RIT MAV Platform Project Review. 2009 MAV Team Members. Basic Project Information. Project Number and Name P09123 Micro Aerial Vehicle (MAV) Platform Project Family Micro Aerial Vehicle Track Aerospace Systems and Technology Start Term 2009-1 End Term 2009-3

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P09123 – 2009 RIT MAV Platform Project Review

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  1. P09123 – 2009 RIT MAV PlatformProject Review

  2. 2009 MAV Team Members

  3. Basic Project Information Project Number and Name P09123 Micro Aerial Vehicle (MAV) Platform Project Family Micro Aerial Vehicle Track Aerospace Systems and Technology Start Term 2009-1 End Term 2009-3 Faculty Guide Dr. Jeffery Kozak (Mechanical Engineering) Faculty Consultants Dr. Agamemnon Crassidis (Mechanical Engineering) Dr. Hany Ghoneim (Mechanical Engineering) Primary Customer Dr. Jeffery Kozak, RIT MAV Team Secondary Customer Impact Technologies

  4. Product Description /Project Overview Mission Statement: The MAV Family of Projects: To build a semi-autonomous, tending towards full autonomy, air vehicle that will be used in the future for Multidisciplinary Senior Design and for graduate studies in the college of engineering and the college of imaging science. To have a hands on aeronautical project for undergraduate students that is of low cost and simplicity as to be able to be made by hand. To provide an incentive for students as well as exposure of engineering at RIT by competing in the more aggressive United States/Europe MAV competition The P09123 Project will: Develop the Platform for an expandable and re-useable Micro Aerial Vehicle (MAV) that is intended to be used as a basis for current and future MAV design.

  5. Basic Subsystem Layout – “The Diagram” Tail Assembly: -Vertical Stabilizer -Horizontal Stabilizers -Control Servos Fuselage Wing Assembly (2): -Airfoil -Control Surfaces -Control Servos Equipment Cage: -R/F Electronics -GPS -Microcontroller -Batteries Nose Cone Assembly: -Propulsion -Motor/Controller -Propeller

  6. MAV Subsystem Architecture • Propulsion • Thrust Requirements • Propeller • Motor and Controller • Nose Cone Design • Control Surfaces • Servo Actuation • Size, Shape, Function • Material • Location • Fuselage • Material/Construction • Structure • Integration • Wings/Airfoil • Airfoil Shape • Tail Design • Flight Dynamics • Aerodynamics • Material/Construction

  7. MAV Subsystem Breakdown • Process Development • Manufacturing Process • Final Assembly • Documentation • Procurement • Bill of Materials/Cost Analysis • Analysis/Testing • Flight Testing • Wind Tunnel Testing • CFD/FEA • Material Testing • Simulation • Equipment Cage • Structural Integrity • Hardware Mounting • Protection • Vibration Damping • Electronics • Batteries • R/C Elements • Motor Controller • Power Requirements • Servo Control

  8. Performance • Cruise speed = 25 mph • Max Speed = 60 mph • LiftTotal = 3.31 lbf at cruise • DTotal = 1.28 lbf at cruise • ThrustTotal = 3.627 lbf with 90% efficiency • Tentative Flight Time = 10 mins • Conservative estimate • Will be fully tested once built in MSD II

  9. 2009 MAV Fuselage Tapered Tail End to Reduce Drag Force Material: Carbon Fiber/Kevlar Biaxial Sleeve Wing Attachment Points Cage Structure Housed in Body

  10. Safety Issues

  11. Weight Summary

  12. Bill Of Materials

  13. MSD IIConcept Development- Project Schedule

  14. MSD IIConcept Development- Project Schedule

  15. Risks • Propeller Dangers • Wing attachment • Manufacturing Tolerances • Weight • Cage • Servos • Batteries • Wing Reinforcement Material

  16. THANK YOU

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