Single Line Tethered Glider System Level Design Review Team P14462 - - PowerPoint PPT Presentation

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Single Line Tethered Glider System Level Design Review Team P14462 - - PowerPoint PPT Presentation

Single Line Tethered Glider System Level Design Review Team P14462 Kyle Ball Jon Erbelding Matthew Douglas Paul Grossi William Charlock Sajid Subhani Team Introduction Team Member Major Sajid Subhani Industrial Engineer - Team Lead


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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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11/2/2013 Systems Level Design Review P14462

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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11/2/2013 Systems Level Design Review P14462

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 design Biege: DAQ Grey: Test flight White: 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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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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Art’s Plane

  • Sustained multiple damages
  • Gained crash experience
  • Possible tethered flight concept

tests

  • Salvage parts
  • Sorry Art 
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Glider Concepts

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Buy Glider

Pros:

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

Bixler 2 Airwing WingSurfer Sky Eye Phoenix 2000

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Build Glider

Pros:

  • 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 Gyro

Pros:

  • 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 Cells

Pros:

  • Can repair individual

components

  • Accurate
  • Cheap Components

Cons:

  • Difficult to calibrate
  • Potential for noisy data
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3-Axis Load Cell

Pros:

  • Accurate
  • Precalibrated
  • Intuitive Setup

Cons:

  • Expensive
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IMU Board and 1-Axis Load Cell

Pros:

  • 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 GPS

Pros:

  • 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 Station

Critieria 3 Single Axis Load Cells 3-Axis Load Cells Force Gauge and GPS Force Gauge and Resistance Gyro IMU and Load Cell 2 Potentiometers and Load Cell Clean Appearance +

  • +

s Number 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 s Is Durable s

  • s
  • Data Acquisition

s

  • s

s Weight s

  • s
  • +

Tension Resolution + s s s s Direction Resolution +

  • +

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

  • 3
  • 9

3 3 Datum Concept Options

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Pugh Diagram – Base Station

Critieria 3 Single Axis Load Cells 3-Axis Load Cells Force Gauge and GPS Force Gauge and Resistance Gyro IMU and Load Cell 2 Potentiometers and Load Cell Clean 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 s Is Durable + + + + + Data Acquisition s s

  • s

Weight

  • Tension Resolution

s + s s s Direction Resolution

  • s

Sum of "+" 4 7 4 2 6 Sum of "s" 5 3 3 5 5 Sum 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 ($) Glider Glider 100 Receiver 60 Battery x2 40 Base Station Materials 100 Electronics 100 Total 400 Remaining (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?