M-SAT Missouri S&T Satellite Team SHOT II Pre-Launch Ryan Pahl Matt Campbell Stephanie Evans Austin Ferguson.

Slides:



Advertisements
Similar presentations
Design and Implementation of Low- Cost Optical Telemetry to Support Radiometric Analysis of the Atmosphere University of Colorado at Boulder Alexandra.
Advertisements

Cornell University Space Systems Design Studio AIAA GNC Conference - 8/11/2009 Violet: A High-Agility Nanosatellite for Demonstrating Small Control-Moment.
Cornell University Space Systems Design Studio AIAA GNC Conference - 8/11/2009 Violet: A High-Agility Nanosatellite for Demonstrating Small Control-Moment.
1 Electrical and Computer Engineering Cameron Proctor Ramsey Khudairi Thomas Gilbert Chad Young MDR Presentation TekBand.
Gary MKIII University of Central Florida Chris Valle, Braden Urban, John Rowe, and Tyler Yoemans.
Adam Archuleta Katie Cartee Logan Farley Patrick Klein Kamron Medina Catherine Villa TEAM INFINITY AND BEYOND LAUNCH READINESS REVIEW Fall 2011 Rev C
Brynn Larson Trey Karsten Terek Campbell Marcus Flores Marcell Smalley Shunsuke Miyazaki 2015/6/10 Team Ochocinco.
CASTOR Jr. MIT 2LT Corey Crowell 2LT Matt McCormack Lucas de la Garza Spenser Parra.
BEARSat Thermal Switch University of Cincinnati Josh Cory Jacob Hause Eric Riedl Matt Urbainiak University of Cincinnati Josh Cory Jacob Hause Eric Riedl.
- The Organizers Introductions: Student Hands On Training Workshop II Workshop Student Hands On Training Workshop II Workshop Boulder, Colorado June 11.
STARLight PDR 3 Oct ‘01J.1 Miller STARLight Electrical Ground Support Equipment Ryan Miller STARLight Electrical Engineer (734)
Baby SAT University of Missouri-Rolla Carl Seubert Jason Searcy Joshua Jacobs Michelle Rader.
BOREAS: Balloon Sub-Orbital Radio Evaluation of Data TransmissionSlide 1 of 6 6/14/2006 Introduction:
1 SHOT II Communication System Experiment University of Minnesota Max Schadegg, Cole Christensen, Ian Macmillen, Steve Haviland June 10 th, 2010 University.
Safeguarding the Three Corner Sat Constellation By Stephen Levin-Stankevich Stephen Nauman.
Christian Zempel Eric Stackpole Gavin Hagiwara Xander Wroblewski Department of Mechanical Engineering IRIS-VIEWS SHOT II 6/11/10 Verification of In-flight.
M-SAT Missouri S&T Satellite Team SHOT II Post-Launch Ryan Pahl Matt Campbell Stephanie Evans Austin Ferguson.
Cube Root Georgia Institute of Technology Matt Bigelow, Gregory Hansen, Sarah McNeese, Luke Walker.
Texas A&M University Ryan Goodnight Amanda Collins Libby Osgood.
Minnesat SHOTII Presentation, June 16 th, Minnesat University of Minnesota Jason Mintz Jim Pogemiller Abdul Azeem Khan Vincent Jusuf SHOT II Presentation.
Mission Expectations As Planned: –Full end-to-end test of Akoya-Bandit imaging and dedicated comm subsystems –Take, store, and transmit images over 900MHz.
Team DSRO Critical Design Review Taylor Boe Andrew Buckner Andrew Gilbert Emily Howard Grace Harsha Bobby Stillwell October 14, 2008.
Launch Readiness Review 11 Nov Brady Phillips, Elliot Guber, Brandon Campbell, Dushyant Dhundra, Joel Mendez, Cameron Trussell.
Bronco 1 Casey Kute Phelps Williams Kuan Ju Ho Kyle Ogle.
Space Debris Launch Readiness Review Seanna Renworth, Emily Logan, Corey Godwin, Sean Murphy, Cole Bostrom, Jonathan Kirchmaier November 11 th, 2008.
What is GPS? GPS, which stands for Global Positioning System, is the only system today able to show you your exact position on the Earth anytime, in any.
 A data processing system is a combination of machines and people that for a set of inputs produces a defined set of outputs. The inputs and outputs.
COMPONENTS OF THE SYSTEM UNIT
University at Buffalo GLADOS SHOT II Balloon Payload Presentation June 29, 2012 Andrew Dianetti, Alex Wende, Bryant Carlson, Joe Flannery 1.
Argus: SLU Core Bus Operational Test Steve Massey, Tyler Olson, Joe Kirwen, Wesley Gardner SHOT II Pre-Launch Presentation June 29, 2012.
TERSat Massachusetts Institute of Technology Eric Peters, Danilo Roascio, Leonard Tampkins, Kezi Cheng July 1st,
DEC0905 Remote Control of Home Appliances ABSTRACT The objective of this project is to enable users to remotely control home appliances and systems over.
DemoSat IV Critical Design Review Metropolitan State College of Denver April 21, 2006.
Balloon Fest December 7, 2013 Team 26 Learning for Life School Group 3 – Wolves (Advanced) Determine Whether GPS Altitude Lags Barometric Pressure and.
Objectives Overview Discuss the purpose of the components required for successful communications and identify various sending and receiving devices Differentiate.
Scott Coffin Adam Faucher Jason Graika Brian Voelz Client: Honeywell Advisor: Dr. Zhengdao Wang.
Group Members Mike Svendsen – Computer Engineer Steve Towey – Computer Engineer Brian Walker – Architect Richard George – Industrial Technology Client.
Atomic Aggies CDR. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: inches Approximate Loaded Weight: lb.
Moving from paper to electronic prescriptions An overview of Electronic Prescription Service Release 2.
Flight Testing Small Satellites Through High Altitude Ballooning Presented by Zach Henney 18 April 2015.
1 University of Maryland DYMAFLEX SHOT II Pre-Flight Presentation June 29, 2012.
Boston University Daniel TaylorNima Badizadegan R. Terry BlackPantelis Thomadis.
Bully Blue Lock Midterm Presentation 2014 Senior Design II.
Aerospace Digital Communication Instrument Senior Design 1 Presentation.
M-SAT Missouri University of Science & Technology SHOT II June 29 th 2012 Caleb Myers Levi Malott Keith LeGrand Matt Glascock.
Victor Taberski, Ryan Walker, Allen Marshall, Matt Kerwin, Andrew Winthrop, Steven Ramm October 14, 2008 UANIOOU – (Upper Atmosphere Near-Infrared Optical.
MSU SeaMATE ROV Explorer Class
Prox-0.3 Georgia Institute of Technology Kiichiro DeLuca Richard Zappulla Matt Uhlman Ian Chen 1.
University Nanosat -6 Program Allison Cook – Project Manager, Structure, Flight Test Brian Verbus – Systems, Structure Kerry Fessendon – Structure, Flight.
TERSat Massachusetts Institute of Technology Eric Peters, Danilo Roascio, Leonard Tampkins, Kezi Cheng June 29,
University at Buffalo GLADOS SHOT II Balloon Launch Results Presentation July 1, 2012 Andrew Dianetti, Alex Wende, Bryant Carlson, Joe Flannery 1.
BANDAGE SIZE NON ECG HEART RATE MONITOR USING ZIGBEE WIRELESS LINK Guided by,Presented by, Ms. Geo. P.G Jeevan.K.Noble Asst.Prof., ECE Dept.S7, ECE-A.
MY NEST A TECHNOLOGICAL OVERVIEW. NECKLACE Reason: Hidden Less like being tagged and branded (jail)
Boeing NFC Part and Process Tracking System Team 41 Alper Olcay – Vigneshwar Karthikeyan – Jinjoo Nam.
CHAPTER 8 Communication and Network Copyright © Cengage Learning. All rights reserved.
Jeremy Sandoval University of Washington May 14, 2013
Junk in a Box Critical Design Review
CanSat Competition Competition Objectives Pre-Launch Launch
Accelerometer-Based Character Recognition Pen
CUSat High Altitude Test (CHAT) Mission Briefing
Mike Pappas, Nigel Himmelreich, Eric Anderson
StratoBuoy II Matt Voll Brian Mayernik Pat O’Hara.
Mike Pappas, Nigel Himmelreich, Eric Anderson
HA1L High Altitude 1U Laboratory
Orbital Debris Detector Sensor Subsystem
University of Maryland DYMAFLEX SHOT II Post-Flight Presentation
FRIDAY SLIDES TEMPLATE
Accelerometer-Based Character Recognition Pen
<Your Team # > Your Team Name Here
Presentation transcript:

M-SAT Missouri S&T Satellite Team SHOT II Pre-Launch Ryan Pahl Matt Campbell Stephanie Evans Austin Ferguson

2 Mission Overview The main purpose of this mission is to test the Bluetooth technology used to communicate data between MR and MRS SAT Compare the data sent and data received after recovery to determine success/failure rate

3 SHOT II / UN-6 Connection M-SAT consists of two separate satellites that will communicate using Bluetooth technology During the UNP-6 mission, MRS SAT’s GPS position data will be transmitted via Bluetooth to MR SAT where MR SAT will process the data for formation control purposes Verify Bluetooth operation over extended range

4 SHOT II Design and Test Details Each payload will contain a microcontroller and Bluetooth module –The microcontroller has an 8051 architecture –The Bluetooth module is a BlueGiga WT11-E Modules hidden to prevent interference During the testing, the prototype box proved that it was capable of surviving the extreme stress that may take place during the mission –~545 g per sat –Whip test –Drop test –Stair test

5 Expected Results The two payloads should be able to communicate throughout the mission –The transmitting box sat will send a string of characters in a repeating pattern to the receiving box sat –The transmitting box will record the number of characters sent and the receiving box will store the actual characters for later comparison A ground range test was performed and the boxes functioned to a distance of 155 m

6 Demonstration The two boxes will be separated to test the range of the Bluetooth A light has been placed on each box to display when the boxes are connected and transmitting