Cansat 2008: University of Michigan Victor V Final Presentation

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1 The University of Michigan CanSat Victor_V Final Presentation June 15, 2008 1

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Final presentation by the University of Michigan Victor V team at CanSat 2008http://www.astronautical.org/2008/06/15/cansat-2008-university-of-michigan-victorv/

Transcript of Cansat 2008: University of Michigan Victor V Final Presentation

Page 1: Cansat 2008: University of Michigan Victor V Final Presentation

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The University of MichiganCanSat Victor_V

Final PresentationJune 15, 2008

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CanSat Overview

Kelert Bizbiqi

CanSat OVERVIEW > CONOPS > Data Results > Lessons Learned

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CanSat DesignCanSat OVERVIEW > CONOPS > Data Results > Lessons Learned

Kelert Bizbiqi

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Actual CanSatCanSat OVERVIEW > CONOPS > Data Results > Lessons Learned

Kelert Bizbiqi

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System DiagramCanSat OVERVIEW > CONOPS > Data Results > Lessons Learned

Kelert Bizbiqi

Receiver/Modem Cansat

MODEM5V

Logomatic5V

MPU

AT

MEL

Atm

ega1

682.

35V-

3.6V

BATTERYLithium

7-9V

GPS3.3-5V

VOLTAGE CONVERTER

9V –> 3.4V

VOLTAGE CONVERTER

9V à 5V

Red Wire Servo 5V x2Black wire

Power

Data

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Design Evaluation

Requirement CanSat Design Criterion Met

Land Upright Triangular Design Yes

Max. Weight 460 grams Yes

Release Parachute Actuating Legs No

Deploy Parachute Automatic at Separation Yes

Telemetry Data GPS with Datalogger Yes

Max Descent Rate ~4.4 m/s N/a

No Protrusions All housed in Prism Yes

Max Dimensions D: 59.2mm L:261mm Yes

Kelert Bizbiqi

CanSat OVERVIEW > CONOPS > Data Results > Lessons Learned

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Concept of Operations

Kelert Bizbiqi

CanSat Overview > CONOPS > Data Results > Lessons Learned

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Predicted Operation Timeline

Task Time from LaunchArrival -4 hours CanSat Component Testing -3.45 HoursGround Station Assembly -2 hours CanSat Check-In -1.5 Hours Turn CanSat ON -11 minutesRocket Integration -10 minutesBegin Ground Station Data Collection - 6 minutesLaunch Pad -5 minutesInitialize Ground Station Software -4minutesLaunch 0Maximum Altitude ~+11 secondsCanSat Deployment +12 secondsParachute Deployment +14 secondsLanding @ 4.5 m/s +7 minutesData Analysis +10 minutesRecovery of CanSat +15 minutes

Kelert Bizbiqi

CanSat Overview > CONOPS > Data Results > Lessons Learned

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Actual Operation Timeline

Kelert Bizbiqi

CanSat Overview > CONOPS > Data Results > Lessons Learned

Task Time from LaunchCanSat Component Testing -4 hourArrival to Launch Site -1 hourGround Station Assembly -44 minutesCanSat Weigh-in -32 minutesRocket Integration -8 minutesInitialize and Begin Ground Station Data Collection -7 minutesSetup Rocket for Launch -4 minutesTurn on CanSat -4 minutesLaunch 0Maximum Altitude ~+11 secondsCanSat Deployment +12 secondsParachute Deployment +14 secondsLanding @ 4.5 m/s +5 minutesRecovery of CanSat +8 minutesData Analysis +5 hours

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Planned Launch Site Roles

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• Before Launch/During Flight– 2 Spotters

• The spotters will be tasked with the responsibility of tracking the CanSat.• The spotters will be placed in the field away from the tents and ground station.• They will be equipped with binoculars.• The spotters after finding the CanSat will inform the judges and return to the ground station with the payload

– 2 Ground Station Operators• The GS operators will be tasked with orienting the antennas and tracking the data stream into laptop

Kelert Bizbiqi

CanSat Overview > CONOPS > Data Results > Lessons Learned

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Launch Site Roles

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• Before Launch/During Flight– 2 Spotters

• The spotters tracked the CanSat.• The spotters went to retrieve the payload and discovered the battery fell out upon impact.

– 1 Ground Station Operator• The GS operator monitored the telemetry data transferred to the computer. The data stopped upon launch.• The data was lost, when another connection was tried to be established.

Kelert Bizbiqi

CanSat Overview > CONOPS > Data Results > Summary > Lessons Learned

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Planned Launch Site Roles

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• After Launch– 2 Flight Team members (Spotters)

• One engineer will analyze the data coming in through the telemetry and plot the data to see if it is accurate

• The other engineer will analyze the data in the SD Card– The engineer will convert the NMEA sentence to KML and display the

path of the CanSat on GoogleMaps– The engineer will also plot the data to see if it is accurate

– 2 Flight Team members (GS Operators)

• They will pack the equipment and load the van with the supplies the brought to the field

– After completing the listed tasks, the flight team will keep hydrated and assist the competition in locating other CanSats

Kelert Bizbiqi

CanSat Overview > CONOPS > Data Results > Lessons Learned

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Launch Site Events

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• After Launch– 2 Flight Team members (Spotters)

• Recovered the data in the SD Card• Tried to determine what went wrong with telemetry

communications• Helped out the other CanSat team

– All Flight Team members

• They packed the equipment and loaded the car with the supplies brought to the field

Kelert Bizbiqi

CanSat Overview > CONOPS > Data Results > Lessons Learned

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Data Results

Xin Zhang

CanSat Overview > CONOPS > DATA RESULTS > Lessons Learned

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Flight Path

Xin Zhang

CanSat Overview > CONOPS > DATA RESULTS > Lessons Learned

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Altitude

Xin Zhang

CanSat Overview > CONOPS > DATA RESULTS > Lessons Learned

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CanSat Achievements

• Launched and Recovered Successfully• Land in Upright Position• Able to get GPS data from on board SD

memory

CanSat Overview > CONOPS > DATA RESULTS > Lessons Learned

Xin Zhang

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Lessons Learned

Stephen Hickey

CanSat Overview > CONOPS > Data Results > LESSONS LEARNED

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Failure Analysis

• Ground Station lost communication with the CanSat shortly after launch

• Battery detached upon landing • GPS satellite lock failure caused distorted

altitude data

Stephen Hickey

CanSat Overview > CONOPS > Data Results > LESSONS LEARNED

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Lessons

• Match testing environments more closely• Order components early• Use quality equipment (wires, cutters, etc)• Team organization

CanSat Overview > CONOPS > Data Results > LESSONS LEARNED

Stephen Hickey

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Questions?