Carleton University Fixed Wing UAV Project

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Carleton University Fixed Wing UAV Project Prof. Jeremy Laliberté [email protected] http://uav.mae.carleton.ca

Transcript of Carleton University Fixed Wing UAV Project

Page 1: Carleton University Fixed Wing UAV Project

Carleton University Fixed Wing

UAV Project

Prof. Jeremy Laliberté

[email protected]

http://uav.mae.carleton.ca

Page 2: Carleton University Fixed Wing UAV Project

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

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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

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GeoSurv II Prototype

UAV Overview

▪ Geophysical survey UAV

▪ 185lb 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)

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Team Organization –

Matrix Structure

▪ Functional groups

• Mission Analysis and Design Integration

• Aerodynamics

• Structures

• Avionics

▪ Cross-functional groups

• Flight Testing

• Advanced Design

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Major Project Goals for 2013/14

▪ NextGen GeoSurv II (detailed design and assembly)

• Complete re-build of airframe following March 2012 flight attempt

• Develop flight test program

• Ground testing of all systems, taxi testing, flight attempt (Spring 2014)

▪ Corvus Demonstrator and Final Design

• Complete assembly of demonstrator

• Develop flight test program

• Ground, taxi and flight testing (Fall 2013)

• Detailed design of final Corvus – Lessons learned from flight testing

▪ Avionics test beds and Mission Analysis

• ArduPilot and Micropilot hardware and software-in-the-loop simulations

• Detailed mission simulation and planning software development

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What do you get to do?

Air vehicle Design and Analysis

Avionics design and development Integration and Project Management

Manufacturing and Testing

Page 8: Carleton University Fixed Wing UAV Project

Questions?

UAV Project Winter Design Review

18 March – Senate Room