Low Altitude Balloon Experiment in Technology (LABET) Group Members – Richard George – Industrial Technology Mike Svendsen – Computer Engineer Steve Towey.

Slides:

Advertisements

Similar presentations

TEAM 9 - MRAV DESIGN CONSTRAINTS ANALYSIS by Nick Gentry.

Advertisements

Aerial Surveillance Drone Design Review Tuesday, March 12, 2013 Colin Donahue Samantha Kenyon Jason Lowden Benjamin Wheeler.

Eddie McGovern, Adam Blake, Ryan Vogel, Alleyce Watts, and Jade O’Mara.

HumTempII Lisa Caraway Lisa Caraway Samira Henderson Samira Henderson James Mathis Boswyk Offord II Boswyk Offord II Jonathan Siomo Jonathan Siomo Quincy.

Illinois Space Society Tech Team USLI CDR Presentation.

RockSat-C 2012 CoDR Minnesota Sound Wreckers Conceptual Design Review University of Minnesota Alexander Richman Jacob Schultz Justine Topel Will Thorson.

Closing Summary Design Testing Abstract Monitoring crop heath via aerial photography is a proper technique used to maximize agricultural productivity.

Alex Funiciello Dan Graves Mike Hardbarger Jim Reepmeyer Brian Smaszcz May 14, 2010.

Wireless Terminal and PC Interface Using VLSI EE451 - Senior Project Members: Chris Brophy Matt Olinger Advisor: Dr. V. Prasad 12/11/01.

EDGE™ Concept Level Project Plan P08110 – UAV Based Digital Imaging System David Eells (Mechanical Engineering)

1 Design Group 2 Kat Donovan - Team Leader Andrew DeBerry Mike Kinder John Mack Jeff Newcamp Andrew Prisbell Nick Schumacher Conceptual Design for AME.

P09231: Airframe A A. Matt Greco (ME) B. Shawn O’Neil (ME) C. Eric Lannan (ME) D. Will Pisarello (EE) E. Brian Lindquist (IE) F. Phil Davenport (IE)

Field Navigational GPS Robot Final Presentation & Review Chris Foley, Kris Horn, Richard Neil Pittman, Michael Willis.

Final Presentation Nick Hoffmann Miranda Rohlfing Geoff Morgan Miles Buckman Lauren Wenner Rahul Devnani December 5, 2006.

GPS-Guided Autonomous Vehicle.

Conceptual Design Review Nick Hoffmann Miranda Rohlfing Geoff Morgan Miles Buckman Lauren Wenner Rahul Devnani September 21, 2006.

Client: Space Systems & Controls Laboratory (SSCL) Advisor : Matthew Nelson Anders Nelson (EE) Mathew Wymore (CprE)

Improving the Reliability of GPS Tracking Beacons Clayton Jacobs Mentor: Jack Crabtree.

April 26, Team Information Designation Ongo-03 Members Advisors Dr. J. Lamont, Prof. R. Patterson, Dr. Rajagopalan, Dr. J. Basart ClientSpace Systems.

WCBI Team Information Team number: Client: Faculty Advisors: Technical Advisors: Team Members: May02-11 Square D Company (Greg Wiese) Glenn Hillesland.

Internet Piloted Blimp Alfredo Guevara, Jr. Advisor: Professor Spinelli March 1, 2008.

Speed of Sound Team BalloonWorks. Table of Contents Mission Goal and Objectives Science and Technical Backgrounds Mission Requirements Payload Design.

Illinois Space Society Tech Team USLI FRR Presentation.

Client: Space Systems & Controls Laboratory (SSCL) Advisor : Matthew Nelson Anders Nelson (EE) Mathew Wymore (CprE)

AE 1350 Lecture Notes #9.

Google project Loon -Balloon powered internet for everyone

Team Flying Camels Nawar Chaker Paul Savage Tim Jacobs Pete Dokter Adam Swartley Capstone Project January 22, 2005.

The Boeing 777 can hold a max of 550 passengers on board and 2 crew members.

LABET Low Altitude Balloon Experiments in Technology CPR E 491 ENGR 466.

Proposed Approach  Research available commercial satellite communications services  Explore viable battery technologies  Investigate GPS receiver functionality.

Team Balloon Satellite II Multi-Disciplinary Senior Design CSEN 4201 Level II Mid-Term Report 17 October 2003 Mentor: Tony Kim.

Pre-Flight Briefing ANSR-79 Pima Community College 3/28/14 Nick Patzke Gustavo Guerreo Nick Morris Team Members.

Dhruv Patel 12th- Project manager Max Beasley 11th- Systems Engineer Trey Hargett 11th Jonathan Ford 11th Brent Higdon 11th Austin Lambert 11th Jay Chenault.

Computational Mechanics and Robotics The University of New South Wales

Launching Station for Sensor Deployment Team Members: Brian Molnar, Shawn McGrady, Joe Liquore, Ken Schroeder Faculty Advisor: Dr. Jeff Faculty Advisor:

Flight Readiness Review Student Launch Initiative SCS Rocket Team Statesville Christian School April 2, 2008.

Critical Design Review- UCF Jeremy Young Anthony Liauppa Erica Terry, Emily Sachs Kristen Brightwell Gillian Smith 1.

Group Members Mike Svendsen – Computer Engineer Steve Towey – Computer Engineer Brian Walker – Architect Richard George – Industrial Technology Client.

Client: Space Systems & Controls Laboratory (SSCL) Advisor : Matthew Nelson Anders Nelson (EE) Mathew Wymore (CprE)

Advisor: Dr. Edwin Jones 1 Client: Paul Jewell ISU Engineering Distance Learning Facility May01-13 Design Team: David DouglasCprE Matt EngelbartEE Hank.

UCATS - Status Report1 UCATS Unmanned Control & Tracking System Kurt Chewing Jennifer Greene Dave Manley Jeanette Smith John Smith Team DJ 3 K.

Atomic Aggies CDR. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: inches Approximate Loaded Weight: lb.

Tethered Glider - Base Station Group P16462 Sarah Collmus Laura Arciniegas Kevin Collins Aleksandr Kim Michael Ostaszewski Kevin Larkin Sukmin Lee Design.

Aerospace Digital Communication Instrument Senior Design 1 Presentation.

Elliot Penn Will Severynse Nick Proto David Palmer Rebecca Levin Jason Mei.

Smoke Notification System (SNS) Mid-Semester Presentation Senior Design 1 February 28, 2013.

Aerospace Digital Communication Instrument Senior Design Presentation.

Introduction ProjectRequirements Project Requirements In a previous senior design project, a wireless front-end was added to Iowa State University’s Teradyne.

Group Members Richard George – Industrial Technology Mike Svendsen – Computer Engineer Steve Towey – Computer Engineer Brian Walker – Architect Client.

Smoke Notification System (SNS) Final Presentation Senior Design 1 April 18, 2013.

Team 3 Ashwin Shankar Upsham Dawra Samit Sura Joe Katz.

EcpE 492: Dec09-14 Engr 467: LABETIV_SP09 Henri Bai Steve Beckert Ian Moodie Mike Rau Matthew Nelson, Advisor John Basart, Advisor November 19, 2009.

Abstract Each July, the Association for Unmanned Vehicle Systems International holds an annual International Aerial Robotics Competition (IARC), with major.

January 14,  Length: inches  Diameter: 6 inches  Mass: oz. / lbs.  Span: 22 inches  Center of Gravity: inches 

Final Presentation Senior Design II. Ralph Sandford Computer Engineer Focus: Navigation Controls Mike Smith Electrical Engineer Focus: Endurance PCB Design.

Mini Autonomous Flying Vehicle CASDE is part of the National effort to develop a Micro Air Vehicle. CASDE has chosen a Mini Vehicle, in the short term,

Abstract Keeping multiple children safe and accounted for can be a daunting task. When someone loses track of a child, even for a little while, anxiety.

By: Ryan and Drew.  Armament (weapons): None  Engines: Two Pratt and Whitney J58’s (each weighing 6,000 lbs.)  Maximum Speed: Mach 3.2 (3.2 times the.

P07122: Autonomous Quadcopter Jason Enslin – EE: Team Leader, Circuit Design/Testing Glenn Kitchell – CE: Programming, Software Design Richard Nichols.

P07122: Autonomous Quadcopter Jason Enslin – EE: Team Leader, Circuit Design/Testing Glenn Kitchell – CE: Programming, Software Design Richard Nichols.

EDGE™ Preliminary Project Plan P09102 – METEOR Stage Separation System JJ Guerrette (ME)

Smoke Notification System (SNS) Mid-Semester Presentation Senior Design 1 February 28, 2013.

Inertial Measurement Unit. Project Advisor: Dr. Basart Client: Matt Nelson Team Members (491): Matt Ulrich Luis Garcia Amardeep Jawandha Julian Currie.

Low Altitude Balloon Experiment in Technology (LABET)

Critical Design Review Presentation

PROJECT METEOR: RITSAT1 P08102

Image Acquisition and Processing of Remotely Sensed Data

P07122: Autonomous Quadcopter

Rudra Timsina Micah Lucas Marc Salas Advisor: Richard Messner

Presentation transcript:

Low Altitude Balloon Experiment in Technology (LABET) Group Members – Richard George – Industrial Technology Mike Svendsen – Computer Engineer Steve Towey – Computer Engineer Brian Walker – Architect Advisor – Matt Nelson

Project Description The LABET project has been an ongoing project with the Space Systems and Controls Lab (SSCL) that aims at developing a blimp that can be flown for research and for outreach events for the SSCL. Past LABETs have been designed for indoor use only. This project aims to develop a blimp system that can be flown in outdoor conditions with winds under 10 mph. Objective – – Develop a new LABET frame – Develop new LABET avionics

Requirements D/WRequirement DR1. The LABET will fly at a maximum altitude of 500 feet. DR2. The communication range shall be at least 1 mile. WR3. The communication range should be at least 2 miles. DR4. The LABET shall have a remote control. DR5. The LABET shall have a weight of under 5 pounds. DR6. The LABET electronics shall have a weight of under 1.5 pounds. DR7. The LABET shall be able to carry a payload of 200 grams. DR8. The LABET shall operate in wind speeds of up to 5 mph. WR9. The LABET should operate in wind speeds of up to 10mph. WR10. The LABET should be able to take and send video to a ground station. DR11. The LABET shall have a flight time of 30 minutes. DR12. The LABET shall have a pressure sensor to determine altitude. DR13. The LABET shall have a GPS module to determine position. DR14. The LABET shall have a rate gyro to keep it flying straight

Constraints and Technical Considerations All motors, electronics, and batteries must weigh under 1.5lbs. The motors must provide enough thrust to overcome 10 mph winds. Obtaining a small RF device that is still able to broadcast up to 2 miles.

On Board System Diagram

Frame Design

Balloon Design

Tasks/Schedule

Risks and Mitigation RiskMitigation Schedule too aggressiveThe timeline for the subtasks is aggressive, but each overall task has extra time allocated for unexpected setbacks. Lack of experience with RC devices.Research online and work closely with advisor. Parts not performing as expected.Account for this and purchase slightly “overpowered” motors, so if they under perform requirements are still met. Little experience with circuit board design and fabrication. Work closely with advisor.

Cost Estimate

Questions?