Single Line Tethered Glider

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9/30/2013 Systems Level Design Review P14462 Single Line Tethered Glider Team P14462 System Level Design Review Jon Erbelding Paul Grossi Sajid Subhani Kyle Ball Matthew Douglas William Charlock

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Single Line Tethered Glider. System Level Design Review. Team P14462. Kyle Ball Matthew Douglas William Charlock. Jon Erbelding Paul Grossi Sajid Subhani. Team Introduction. Agenda. Project Description Review Customer Needs Review Customer Requirements Review - PowerPoint PPT Presentation

Transcript of Single Line Tethered Glider

Page 1: Single Line Tethered Glider

9/30/2013 Systems Level Design Review P14462

Single Line Tethered Glider

Team P14462System Level Design Review

Jon ErbeldingPaul Grossi

Sajid Subhani

Kyle BallMatthew DouglasWilliam Charlock

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Team Introduction

Team Member Major

Sajid Subhani Industrial Engineer - Team Lead

Paul Grossi Mechanical Engineer

Matt Douglas Mechanical Engineer

Jon Erbelding Mechanical Engineer

Kyle Ball Mechanical Engineer

Bill Charlock Mechanical Engineer

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Agenda● Project Description Review● Customer Needs Review ● Customer Requirements Review● Functional Decomposition● Concept Development● Concept Comparison● Data Collection Architecture ● Risk Assessment● Project Planning● Work Breakdown Structure

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Project Description● Goal: Design, build, and test a tethered,

small-scale, human-controlled glider.

● Critical Project Objectives:○ Maintain maximum tension on the tether○ Sustaining horizontal and vertical flight

paths○ Measure and record tether tension and

position○ Understand the influential parameters for

sustained, tethered, unpowered flight

Glider

Tether

Base Station

Operator w/controller

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Customer Requirements

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Engineering Requirements

Yellow: Major designBiege: DAQGrey: Test flightWhite: System environment

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Functional Decomposition

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Functional Decomposition

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Functional Decomposition

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Functional Decomposition

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Art’s Plane

● Sustained multiple damages● Gained crash experience● Possible tethered flight concept tests● Salvage parts● Sorry Art

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Concept Development● Gliders

○ Buy an RC glider○ Design and build an RC glider

● Measurement Devices on Base Station○ Buy a 3-axis Load Cell○ Build Load Cell from three 1-axis Load Cells○ GPS with Force Gauge○ Resistance Gyro with Force Gauge○ IMU with 1-axis Load Cell

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Glider Concepts

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Buy GliderPros:● Pre-Engineered to Fly● Can purchase spare parts● Fast shipping● Modifiable

Cons:● Not guaranteed to fly with

tether● Expensive● Limited modifications

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Benchmarking (Buy)Plane Price ($)Bixler v1.1 EPO 1400mm - (ARF) 56.70Hobbyking Bixler 2 EPO 1500 mm w/ Brushless Motor, Servos and Optional Flaps (ARF) 69.99AXN Floater-Jet w/ Servo, Motor, ESC (EPO) PNF 65.22Hobbyking Sky Eye EPO FPV/Glider w/ Flaps 2000mm (PNF) 120.33Phoenix 2000 EPO Composite R/C Glider (Plug and Fly) 78.72Airfield Giant Convertible EDF Power RC Glider Almost Ready to Fly 2400mm Wingspan 209.95Airwing RC WingSurfer Airplane Glider 4 Channel Almost Ready to Fly RC 1400mm Wingspan 79.95Airwing RC Bobcat 6 Channel Pusher Plane RC Kit 1143mm Wingspan 149.95TT-62 Alekto Electric Twin-Engine Fiberglass RC Airplane Kit 127.40

Bixler 2

Airwing WingSurfer

Sky Eye

Phoenix 2000

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Build GliderPros:● Can optimize plane for

tethered flight● Build spare sparts● Resources available

Cons:● Not guaranteed to fly● Requires time to build● Complex● Hard to balance● Could become expensive if

mistakes are made

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Benchmarking (Build)

● Experimental Airlines tutorials (Photon Model as baseline)

● Custom/interchangable design (wing, fuselage, rudder, etc.)

● ~$80 - $100 (~50%-70% “1 time cost”)

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Measurement Concepts

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Force Gauge and Resistance GyroPros:● Innovative

Cons:● Expensive● Complex Data● Internal Turbulence● Requires current line on

tether● Difficult to calibrate● Difficult to set up

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3 Single-Axis Load CellsPros:● Can repair individual

components● Accurate● Cheap Components

Cons:● Difficult to calibrate● Potential for noisy data

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3-Axis Load CellPros:● Accurate● Precalibrated● Intuitive Setup

Cons:● Expensive● Dead zones

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IMU Board and 1-Axis Load CellPros:● Provides accurate position

and orientation data

Cons:● Requires noise filtering● Difficult to calibrate● IMU system would be on

glider

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Force Gauge and GPSPros:● Digital Data● Accurate force measure

Cons:● Expensive● GPS on glider changes

weight● Difficult to calibrate● Difficult to set up● Innacurate position

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2 Potentiometers and 1-Axis Load Cell

Pros● Inexpensive● Accurate angles

Cons● Easily breakable● Require precise

machining

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Pugh Diagram – Base StationCritieria 3 Single Axis Load

Cells3-Axis Load Cells Force Gauge and

GPSForce Gauge and Resistance Gyro

IMU and Load Cell 2 Potentiometers and Load Cell

Clean Appearance + - - + sNumber of Components + + + + -

Setup Time + + - + -Setup Procedure + + - - -

Calibration s - - s +Cost - - - + +

Precision + + - + +Accuracy + + - + +

Spare part Cost - - - - +Spare part Availabilty s s s s s

Safety s s s s sIs Durable s - s - -

Data Acquisition s - - s sWeight s - s - +

Tension Resolution + s s s sDirection Resolution + - - + +

Sum of "+" 8 5 1 7 7Sum of "s" 6 3 5 5 5Sum of "-" 2 8 10 4 4

Total 6 -3 -9 3 3

Datum

Concept Options

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Pugh Diagram – Base Station

Critieria3 Single Axis Load

Cells3-Axis Load Cells

Force Gauge and GPS

Force Gauge and Resistance Gyro

IMU and Load Cell2 Potentiometers

and Load CellClean Appearance s + - - +

Number of Components + + + + +Setup Time + + + s +

Setup Procedure + + + s -Calibration - - - - -

Cost - - - - -Precision - + - - +Accuracy - - - - +

Spare part Cost - - - - -Spare part Availabilty s s s s s

Safety s s s s sIs Durable + + + + +

Data Acquisition s s - - sWeight - - - - -

Tension Resolution s + s s sDirection Resolution - - - - s

Sum of "+" 4 7 4 2 6Sum of "s" 5 3 3 5 5Sum of "-" 7 6 9 9 5

Total -3 1 -5 -7 1

Concept Options

Datum

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Top 3 System Concepts

3 Single Axis Load Cell IMU with Single Axis Load Cell 2 Potentiometers with Single Axis Load Cell

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Data Collection Architecture● Data acquisition: LabVIEW or Arduino● Storage: SD Card or Laptop

Parameter Marginal Value Ideal Value Units

Data Sampling Rate 100 500 Hz

Tension Resolution 0.1 0.01 N

Angular Position Resolution 0.5 0.1 deg

Data Collection Requirements:

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Preliminary Budget Outline

Purchase Price ($)

GliderGlider 100Receiver 60Battery x2 40

Base StationMaterials 100Electronics 100

Total 400Remaining (For Mistakes and Repairs) 100

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Risk Assessment (Full)

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Risk Assessment (High Risk)

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Project Planning

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Project Planning

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Work Breakdown Structure● Paul: Glider Dynamics & IMU Implementation● Jon: Glider Dynamics & Load Cell

Implementation● Kyle: EDGE & Load Cell Implementation / Base

Station Construction● Matt: Glider Dynamics, Purchased Gliders

Analysis & Potentiometer Implementation● Saj: DOE Research & Team Management● Bill: Built Glider Analysis & DAQ

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Questions?