team flying camels nawar chaker paul savage tim jacobs pete dokter adam swartley capstone project...

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Team Flying Camels Nawar Chaker Paul Savage Tim Jacobs Pete Dokter Adam Swartley Capstone Project January 22, 2005

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Team Flying Camels

Nawar Chaker

Paul Savage

Tim Jacobs

Pete Dokter

Adam Swartley

Capstone Project

January 22, 2005

Team Flying CamelsCapstone Project

Driftsonde System Overview

The National Center for Atmospheric Research, NCAR, currently has a project involving a high altitude pressure balloon that periodically drops sensors from a payload

These sensors are used to measure pressure, temperature, humidity and wind speed from a height of 60,000 feet down to the surface

These sensors send data back to the payload, which then relays to an iridium satellite and then finally transferred to a ground station

The project currently is successful, with flight times of three days and twenty sensors

Team Flying CamelsCapstone Project

Driftsonde System

ATLANTIC OCEAN

Zero-pressureB alloon

G ondola(24 sonde capacity)

6 hoursbetw eendrops

NORTHAMERICA

EUROPE

O rbC om mLEO S ate llite

Iridium

LEO Satellite

Gondola

(20-40 sonde capacity) ~16km

50-100 mb

© 2004 Copyright University Corporation for Atmospheric Research

Team Flying CamelsCapstone Project

© 2004 Copyright University Corporation for Atmospheric Research

Team Flying CamelsCapstone Project

Driftsonde ComponentsFlight train

1. Low cost polyethylene zero-pressure balloon (365 m3 & 2,265 m3)2. Parachute3. Radar reflector4. Aircraft Transponder5. Gondola

• Embedded Computer• GPS Navigation System• Flight level PTH sensor• Ballast System• Lithium battery power system• Iridium, global coverage

2-way satellite system• Dropsondes

© 2004 Copyright University Corporation for Atmospheric Research

Team Flying CamelsCapstone Project

© 2004 Copyright University Corporation for Atmospheric Research

Team Flying CamelsCapstone Project

© 2004 Copyright University Corporation for Atmospheric Research

Team Flying CamelsCapstone Project

NSF THORPEX Briefing, D. Parsons, 11/21/03© 2004 Copyright University Corporation for Atmospheric Research

Team Flying CamelsCapstone Project

Excessive weight

Battery Weight

Heavy release mechanism

Battery life limits flight times to 3-5 days

Twenty sondes maximum per gondola

Current System limitations

Team Flying CamelsCapstone Project

Driftsonde Main Goals

Extend flight time

Increase maximum number of sondes to fifty

Balloon size must remain the same

Team Flying CamelsCapstone Project

Proposal

Increase the available power by utilizing renewable energy sources, possibly solar

Decrease the weight of the gondola by decreasing the weight of the power system, i.e. batteries

Implement a monitoring system for the battery health

Streamline a release mechanism to conserve weight

Team Flying CamelsCapstone Project

Power SystemOptions:

Solar: Simplest

Generator: Heavy

Kinetic: Not enough energy

Non-rechargeable batteries: Limited life span

Team Flying CamelsCapstone Project

Power System

Block diagram

SolarPanels

Power Conversion

Battery System

Team Flying CamelsCapstone Project

Power SystemConstraints

1. Cost: $200 materials only2. Total weight 3Kg3. Environment

inside: -20C to +40Coutside: -60 to +40,60,80C

4. Duration Scale from 4 - 10 days operation5. Operate at 50,000 to 80,000 feet (look at from a pressure standpoint)6. System Electronics

    a. IRIDIUM (5V)    b. Transponder (12V) (only operates below 48,000 feet) High power device    c. System electronics (5V)    d. Peak current (during drop of sondes) approximately 1.7 A

7. System health monitoring (if something goes wrong tell us what happed)    battery voltage    solar power voltage    charge current  discharge current

8. Operate independent on ground for 24 hours (14 A-hrs battery capacity)

Team Flying CamelsCapstone Project

Health Monitor System

Monitor battery voltage

Solar power voltage

Charge current

Discharge current

Team Flying CamelsCapstone Project

Release MechanismOptions

Wireless RF : Expensive

Wireless Induction: Simple and feasible

Daisy Chain Bus: Simplest, but possibly heavy

Team Flying CamelsCapstone Project

Release MechanismWireless Induction block diagram

Balloon Control TX Processor Driver TX Coil

RX Coil Envelope Detector RX Processor

Team Flying CamelsCapstone Project

Release Mechanism

Daisy Chain block diagram

Balloon

Sonde 1 Sonde 2 Sonde 3

CANBUS (?)

Element Burn (?)

Team Flying CamelsCapstone Project

Release MechanismConstraints

1. Control 50 Sondes!

2. Cost:

$5 per sonde maximum

$25 per Gondola maximum

3. Functions:

Capable to turn sondes on or off and during drop always on.Turn on for testing in the field then turn off.

4. Cut the sondes from package

5. Command only one sonde at a time - power it release it

Team Flying CamelsCapstone Project

Project ConsiderationsEconomic Aspects

Environmental impact

Sustainability

Manufacturability

Safety

Impact on society

Team Flying CamelsCapstone Project

Economic AspectsWill be used as a research item, so no real marketability

Ball park figure for complete full system: $475 (Parts only)

Team Flying CamelsCapstone Project

Environmental ImpactGondola is reusable

Sondes are expendable and lost

Environmental impact of sonde electronics is considered negligible

Team Flying CamelsCapstone Project

Sustainability and ManufacturabilitySystems will be implemented from common parts, insuring a good supply

Batteries may need to be replaced in gondola before flight

Expect system to be robust enough to overcome manufacturing tolerances

Team Flying CamelsCapstone Project

Safety Concerns

Balloon release

Existing safety procedures are already in place

Our system does not introduce any new safety concerns

Low power devices

Team Flying CamelsCapstone Project

Impact on SocietyInformation gathered from sondes assists weather predictions

Team Flying CamelsCapstone Project

Division of LaborSonde Release Mechanism

Paul Savage

Pete Dokter

Power System and System Health Monitoring

Nawar Chaker

Tim Jacobs

Adam Swartley

All team members will be working on each aspect of the project, in order to have a firm understanding of all components

Team Flying CamelsCapstone Project

Gantt Chart

Team Flying CamelsCapstone Project

Project Risks and ContingenciesUnsure if entire system will work together

Unsure if we can interface our changes with their current system

Unsure of power system components, such as battery charging and solar panels

Unsure of temperature and pressure effects on the entire system

Unknown if system will exceed target weight

Unsure of total cost

Plan to have all prototyping done by Milestone II

Work harder and smarter

Team Flying CamelsCapstone Project

Questions/ Comments?