MAE Capstone Design Project
Introduction and Overview
Prof. Jeremy Laliberté
MAE Capstone Project Coordinator
Winter 2012
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Outline
■ Background and administrative information
■ Learning Objectives
■ Project list and sign-up process
■ Individual project summaries and discussion
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Capstone Project
Background
■ Based on Cranfield University Group Design Project
■ Originally two projects (1992)
– Aircraft and Spacecraft
■ Success of team-style projects led to adoption across
Department (early 2000’s)
■ Evolved into multi-year projects often with external
collaborators and links to graduate research
■ Widely emulated (e.g. Ryerson, RMC, Ecole Poly.)
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Administrative Info
■ Capstone Project Coordinator
– Prof. Jeremy Laliberté ([email protected])
– Ext 1128, rm 3148ME
■ Learning Objectives
– Provide a realistic design learning environment to expose
students to the complexities of modern engineering
design processes, tools and practices.
■ Each project has its own “corporate” approach
dictated by the industry-specific design process
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MAE Capstone Design
Project
■ Total of 8 projects aligned to programs/streams
■ Aerospace (AERO 4907A, B, C)
– Fixed Wing UAV, Helicopter UAV and Spacecraft
■ Mechanical (MECH 4907A, B, C)
– Gas turbine, FSAE Hybrid and CUSP
■ Biomedical-Mechanical (MECH 4917A)
– Crash test dummy
■ Sustainable and Renewable Energy (SREE 4907A)
– High efficiency house
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Sign up Process
■ Web-based sign-up (open 26 March-27 April)
– Link to be posted on MAE website and emailed to 3rd year, 4th year
and co-op mailing lists
– Select 1st, 2nd, 3rd preference
■ Sign-up even if you might be on co-op
– In May-June you can decline and postpone to next year
■ Assignments based on:
– Degree program, project needs, scheduling, time of sign-up,
volunteer experience
– Each project will be restricted first to those students in that specific
program/stream then opened up if space/schedule permits
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Selection Website and
Assignment Process
■ Login using Connect
userid/password
■ Time stamped entries
■ List will be posted and
students assigned to
specific project sections
by Dean’s Office when
registration opens up in
June
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Undergraduate Directed Study
MAAE 4917 (0.5 credit)
■ For students seeking additional “research” experience
■ Calendar description:
– Student carries out a study, analysis, and solution of an engineering
problem. Results presented in the form of a written report. Carried out
under the close supervision of a faculty member. Intended for
students interested in pursuing graduate studies. Requires
supervising faculty member and proposal from student.
– Prerequisite: permission of the Department and completion of, or
concurrent registration in, AERO 4907 or MECH 4907.
■ Approach individual faculty in your area of interest first
Carleton University Fixed Wing
UAV Project
Prof. Jeremy Laliberté
http://uav.mae.carleton.ca
What is a UAV?
▪ Uninhabited Aerial Vehicle
• No on-board pilot
– Controlled remotely or autonomously
• Can be very large or very small
• May be less expensive than a piloted aircraft
• Dull, dirty, dangerous jobs
▪ Carleton’s UAVs
• Corvus
• GeoSurv II
• Avionics test beds (ATBs) Carleton University’s GeoSurv II Prototype UAV
Wingspan 4 m [13 ft]
Maximum Takeoff Weight 20 kg [44 lbs]
Cruise Speed 100 km/h [54 kts]
Comms Limited Range 20 km [11 nm]
Endurance 4 hrs (gas)/45 min (LiPo)
Corvus UAV Overview
▪ High performance, long endurance multi-mission
small UAV (<20 kg MTOW)
▪ Fixed wing platform sized for 7.5 kg payloads
▪ Demonstrator under construction
GeoSurv II Prototype
UAV Overview
▪ Geophysical survey UAV
▪ 200 lb MTOW
▪ 60/100 kts cruise speed
▪ 30 hp engine with pusher prop
Magnetometers
in wing tips
Landing gear
Engine
Empennage
Fuselage
▪ All-composite airframe
▪ Partnership with Sander
Geophysics Ltd (SGL)
Team Organization –
Matrix Structure
▪ Functional groups
• Mission Analysis and Design Integration
• Aerodynamics
• Structures
• Avionics
▪ Cross-functional groups
• Flight Testing
• Advanced Design
Major Project Goals for 2012/13
▪ Current GeoSurv II (detailed design)
• Continued flight and ground testing of current prototype
• Lightweight data acquisition system and autopilot integration
▪ NextGen GeoSurv (conceptual and preliminary design)
• “Advanced Design Group” to begin studying new GeoSurv UAV to address
deficiencies in current design
• Two “competing” options to be developed to preliminary design stage – Updated and improved “GeoSurv II Mk2”
– Completely new “clean sheet” design “GeoSurv III”
▪ Corvus (preliminary and detailed design)
• Wind tunnel testing of airframe and propulsion system
• Hardware-in-the-loop ArduPilot autopilot system testing and development
including flight testing on an Avionics Test Bed aircraft
• Complete detailed design, CFD and FEA analysis and manufacturing
What do you get to do?
Air vehicle Design and Analysis
Avionics design and development Integration and Project Management
Manufacturing and Testing
Questions?
UAV Project Winter Design Review
23 March – Senate Room