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Daniel Taylor Nima Badizadegan R. Terry Black Pantelis Thomadis

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Presentation on theme: "Daniel Taylor Nima Badizadegan R. Terry Black Pantelis Thomadis"— Presentation transcript:

1 Daniel Taylor Nima Badizadegan R. Terry Black Pantelis Thomadis
Boston University Daniel Taylor Nima Badizadegan R. Terry Black Pantelis Thomadis

2 Mission 1: Communications
Determine packet loss in near-space environment Measuring rate of packet loss at varying altitudes Proof of concept for status beacon Status beacon will begin when BUSAT is launched, contains vital status information Important part of communications system

3 Data: COMMS Receive text beacon every 2 minutes after powerup
Similar loss to UN-7 comms link Beacons sent: 27 Beacons received: 16 Highest ALT received: ~85k ft. 40% Loss Makeshift Ground Station

4 Failure Analysis: COMMS
Not all packets received Incorrect azimuth & elevation Difficulty in pointing while mobile Payload instability No packets received after touchdown Assumed catastrophic landing

5 Conclusions: COMMS Successful test of beacon
Transmitter worked throughout the entire flight Plan to reevaluate link budget analysis

6 Mission 2: Magnetometer
Testing magnetometer in different thermal environments Determine three orthogonal magnetic field vectors Determine how well the magnetometer will work with interference

7 Data: MAG Only expectation is that values are obtained
113 points expected, actually got 128 data points per axis in flight, 170 points per axis total including launch and recovery wait times Should show that the magnetometer reads values from varying temperatures and altitudes Should be comparable to IGRF

8 Actual Results: MAG All axes in microgauss End of Flight Balloon Burst
y Start of Flight Z x

9 Failure Analysis: COMMS

10 Failure Analysis: MAG Impossible to compare to IGRF, should be compared to a local field rather than a global field IGRF can only be used at a global level Electrically, no failures

11 Conclusions: MAG Successful test of magnetometer reading
Magnetometer worked throughout the entire flight Scientific mission unsuccessful, unable to analyze field for correctness Know that we can read from magnetometer, and we have data to compare to a local field for future accuracy analysis and calibration tests


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