Cansat 2008: University of New Hampshire Final Presentation

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University of New Hampshire Page 1 University of New Hampshir University of New Hampshir CANSAT Final Presentation June 15 th 2008

description

Final presentation by University of New Hampshire at CanSat 2008http://www.astronautical.org/2008/06/15/cansat-2008-university-of-new-hampshire/

Transcript of Cansat 2008: University of New Hampshire Final Presentation

Page 1: Cansat 2008: University of New Hampshire Final Presentation

University of New Hampshire Page 1

University of New HampshireUniversity of New Hampshire

CANSAT Final PresentationJune 15th 2008

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University of New HampshireUniversity of New Hampshire

WildCatSat Team

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University of New HampshireUniversity of New Hampshire

Outline

• Design Overview• Raw Data Plots• Processed/Analyzed Data Plots• Outcome of Flight Ops/Failure Analysis• Comparison of Actual CONOPS to Planned

CONOPS

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University of New HampshireUniversity of New HampshireMechanical Design Overview

System Bus:• ABS Plastic• Rapid Prototype using 3-D

Printer

Recovery System:• Octagonal Parachute

– Rip-Stop Nylon– Area: 1.016 m2

• Nylon Cord

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University of New HampshireUniversity of New Hampshire

Up-righting System:• Hinged side doors • Torsion springs provide force to open doors• Pin connected to servo motor holds doors in

place/releases doorsParachute Release System:• Pin attached to side door• Pin holds parachute to bus while doors closedTotal Measured Mass: 470g

Mechanical Design Overview

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University of New HampshireUniversity of New Hampshire

Structural Drawings

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University of New HampshireUniversity of New HampshireElectrical System Diagram

ProcessorPressure Sensor

Transceiver

Buzzer Servo

Transceiver

Computer

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University of New HampshireUniversity of New HampshireElectrical Design Overview

Sensors:• SCP1000 Barometric pressure and temp. sensorMicroprocessor:• Atmel ATMega168Transmitter:• Aerocomm AC4790-1000MBattery• 11.1V 800 mAh Li-Poly• 12.26V Initial, 12.19V After Mission: 0.7V Drop

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University of New HampshireUniversity of New Hampshire

Ground Station Computer:• HP Pavilion N5425

Ground Station Receiver:• Aerocomm ConnexLink 4790

Ground Station Antenna:• External high gain omni-directional antenna

Ground Station

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University of New HampshireUniversity of New Hampshire

Raw Data Plots

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University of New HampshireUniversity of New Hampshire

Processed Data

0 20 40 60 80 100 120 140 160 180 2008.4

8.6

8.8

9

9.2x 10

4

Mission Time (s)

Pre

ssur

e (P

a)

0 20 40 60 80 100 120 140 160 180 200-200

0

200

400

600

800

Mission Time (s)

Alti

tude

(m)

Note: Matlab truncation of LS digit = loss in accuracy

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University of New HampshireUniversity of New Hampshire

Processed Data (cont.)

(Processed with Matlab’s ‘Diff’ and ‘Filter’ functions and window size of 10)

From VTI Tech: “Assumed constant temp. gradient of dT/dH from 1976 US Standard Atmosphere”

H = 30°C/(6.5°C/km)*(1-(P/101325Pa)^0.19

20 40 60 80 100 120 140 160 180 2000

1

2

3

4

5

6

7

8

9

10

Flight Time (s)

Des

cent

Rat

e (m

/s)

Reference: VTI Technologies

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University of New HampshireUniversity of New Hampshire

Flight Operations

• Altitude Transmission: Success • Average Descent Rate: 3.3767 m/s• Descent Time: (1340s-1160s)/60 ~3 min

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University of New HampshireUniversity of New HampshireFlight Operations (cont.)

• Recovery: Success• Up-righting System: Success • Ground Temperature (bonus): Not Met

From: 34.48.097N 101.35.244WTo: 34.47.88N 101.35.562W

~1.28km Lateral Distance Traveled

Reference: http://www.movable-type.co.uk/scripts/latlong.html

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University of New HampshireUniversity of New Hampshire

• Pattern Loss ~30%• Ground Absorption• Terrain• Ground Station Antenna height

a) Elev. Pattern b) Azimuth PatternReference: Aerocomm Corp.

Failure Analysis

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University of New HampshireUniversity of New Hampshire

• Satellite activated• Satellite loaded into rocket• Satellite takes initial pressure reading• Rocket launches• Satellite detects pressure change, starts sending pressure/altitude data • Satellite ejects from rocket• Parachute deploys, slowing descent• Satellite descends at less than 4.6 m/s• Satellite continues to transmit data

• Satellite lands• Doors open up-righting satellite• Parachute released• Buzzer activates• Ground temperature reading and transmission• Data transmission stops

Preparation

Launch

Deployment

Descent

Recovery

CONOPS Comparison

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University of New HampshireUniversity of New HampshireWildCatSat Sponsors

– UNH ECE Dept.– UNH ME Dept.

• Jon Arlington at Orbital Sciences Corp.

• The Byrd Family

Todd GrossProfessor and Chair

May-Win TheinAssociate Professor

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University of New HampshireUniversity of New Hampshire

Questions?

Professor May-Win Thein

Project Advisor

Ph.D Mechanical Engineering

[email protected]

Robert TerryTeam Leader

Electrical Engineer

[email protected]