aerospace digital communication instrument senior design 1 presentation

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Aerospace Digital Communication Instrument Senior Design 1 Presentation

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Page 1: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Aerospace Digital Communication Instrument

Senior Design 1 Presentation

Page 2: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Team Members

Alan PritchardComputer Engineering

MCU ProgrammingGUI Design

Brandon HodaTeam Leader

Electrical EngineeringHardware Development

MCU Programming

Reggie RobyElectrical Engineering

Hardware DevelopmentPCB Layout

Page 3: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Overview• Introduction– Problem– Solution

• Constraints– Technical– Practical

• Hardware Block Diagram• Parts and Progress• Timeline

Page 4: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Introduction

• ADCI is a communication device• Used in high-altitude balloons• Will measure temperature, altitude, and

location• Will contain two-way communication device• For Aerospace Engineering Department

Page 5: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Problem

• Current unit is…– Too heavy– Expensive– Consumes too much power

• Only the location is currently transmitted

Page 6: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Solution

• New transmission device– Smaller– Less weight– Less power– Less expensive– More features

Page 7: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Technical ConstraintsName Description

Distance The ADCI must be able to communicate more than 100 miles atground level. It must also communicate at an altitude of morethan 10 miles.

Operating Temperature

The ADCI must operate within a temperature range of -70°C to50°C.

GPS and Altitude Precision

The ADCI must measure location and altitude with a 50-meterresolution.

Temperature Reading Range

The ADCI must accurately measure temperature from -40°C to50°C ± 1.0°C.

Battery Life The ADCI must run on a battery for more than 2 hours undernormal operating conditions; transmitting data at 1 minuteintervals.

Interfacing The ADCI must be able to interface with differentcommunication devices.

Page 8: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Practical Constraints

Name Description

Sustainability Ruggedness The ADCI must be able to survive the flight and the landing of the balloon.

Sustainability Upgradeability The ADCI must use the best sensors in the price range and allow more sensors later.

Page 9: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Ruggedness

• ADCI must survive at high altitude– Low temperature– Water vapor– Wind

• Landing is most important– Impact on hard ground– Dust– Will not protect against water landing

Page 10: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Upgradeability

• Future considerations– Other sensors• Atomic IMU 6 degrees of freedom• Pressure Transducer

– Adding a camera– Control over balloon direction

Page 11: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Hardware Block Diagram

Page 12: Aerospace Digital Communication Instrument Senior Design 1 Presentation

GPS unit• GPS unit is part of Cell module• Sends 5 strings of NMEA data• $GPGGA and $GPRMC strings are used by ADCI

Page 13: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Temperature Sensor

Page 14: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Temperature Sensor

• DS18B20 Digital Temp Sensor (TO-92 Package)• Converts analog voltages to a digital binary signal onboard• Measures Temperatures from -55°C to +125°C (-67°F to +257°F)

Digital Temperature Sensor Diagram [1]

Page 15: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Data Logger

Page 16: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Data Logger

•Vdrive 2 is capable of storing 4GB of data•Uses standard USB flash drive as storage medium•Automatically detects and begins to write to the Jump drive

V2Drive [2]

Page 17: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Battery Information

• Primary Lithium thionyl chloride Battery or Li-S0Cl2• 3.6V per cell.• Use a total of 4 in series to get 14.4V rail• Supply 2400mAh power• Temperature operating range of -55°C to +85°C• Standard AA cell size

Tenergy Battery [3]

Page 18: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Operating Time

• The module uses 90mA while not sending a message• The max current spike measured was 180mA while

sending a message• All currents measured at 14.4V rail

hmA

mAh13

180

2400Worst case battery life:

Page 19: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Cell module

• Sends and receives SMS text messages• Sends GPS NMEA data to MCU• Uses AT&T wireless service• Uses a pre-paid SIM Card for no monthly fee

Terminus cellular module with GPS [4]

Page 20: Aerospace Digital Communication Instrument Senior Design 1 Presentation

NMEA Data• The ADCI reads in NMEA data from the onboard GPS unit• Stores NMEA and sends it as a SMS message

NMEA Data• The ADCI reads in NMEA data from the onboard GPS unit• Stores NMEA and sends it as a SMS message

$GPGGA,001742.735,3326.5143,N,08851.1072,W,1,08,01.0,98.1,M,-28.4,M,,*62

$GPRMC,001741.735,A,3326.5091,N,08851.1169,W,35.10,57.18,071109,,,A*7E

UTC time Latitude Longitude

UTC time Latitude Longitude Speed Date

$GPGGA,001742.735,3326.5143,N,08851.1072,W,1,08,01.0,98.1,M,-28.4,M,,*62

$GPRMC,001741.735,A,3326.5091,N,08851.1169,W,35.10,57.18,071109,,,A*7E

UTC time Latitude LongitudeAltitude

UTC time Latitude Longitude Speed Date

Num of sat.

Page 21: Aerospace Digital Communication Instrument Senior Design 1 Presentation

NMEA to KML Files•THE KML Generator 1.26 used to convert NMEA strings to KML•KML Files are used by Google earth for plotting a Corse

Benefits of KML converter

•Free•Easy to use•Quickly plots traveled Corse

Page 22: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Sample NMEA Code

Page 23: Aerospace Digital Communication Instrument Senior Design 1 Presentation

What’s Left?

• Need a real test flight• More testing to ensure consistent operation

Design II• Design and buy factory PCB• Pressure sensor• External temp sensor• Mount in an enclosure

Page 24: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Timeline

August September October November

Research

Hardware Design

Software

Testing

Prototype Design

Page 25: Aerospace Digital Communication Instrument Senior Design 1 Presentation

References• [1] Maxim IC “DS18B20.pdf". [Online]. Available:

http://datasheets.maxim-ic.com/en/ds/DS18B20.pdf. Accessed November 30, 2009.

• [2] Mouser Electronics “VDRIVE2 FTDI Interface Modules & Development Tools”. [Online].Available: http://www.mouser.com/Search/include/LargeProductImage.aspx?path=ftdi/lrg/vdrive2.jpg. Accessed November 30, 2009.

• [3] Tenergy Battery “Tenergy Primary Lithium thionyl chloride Battery AA Size 3.6”. [Online]. Available: http://www.tenergybattery.com/components/com_virtuemart/shop_image/product/1025d926ca9a7f365a7a443dc6460d07.jpg. Accessed November 30, 2009.

• [4] Terminus “Terminus GSM/GPRS Terminal w/Python and GPS”. [Online]. Available: http://www.semiconductorstore.com/Pages/asp/Item_MoreImages.asp?ItemNumber=GSM864QV1.1. Accessed November 30, 2009.

Page 26: Aerospace Digital Communication Instrument Senior Design 1 Presentation

Questions?