I/O Breakout Board. DEVICE LIST FOR UAV IOB Analog Devices IMU Tyco Electronics GPS Airspeed Differential Pressure Sensor Altimeter Absolute Pressure.

Slides:



Advertisements
Similar presentations
Dan Garber, Jacob Hindle, and Bradley Lan Advisor: Dr. Joseph Driscoll
Advertisements

MicroCART Micro processor C ontrolled A erial R obotics T eam Abstract MicroCART is a group of EE/CprE students tasked with developing an autonomous helicopter.
Critical Design Review ….. Royal Ordnance,Summerfield 17 th February 2001 National Rocketry Competition 2001 Open Rocketry Association Slide 1/14.
Author George Peck EVLA Hardware Monitor and Control PDR March 13, APPLICATIONS AND DEVICE INTERFACE ISSUES.
Inertial Measurement Unit “IMU” (Analog Devices ADIS16350) - Tri-axis gyroscope ± 75°/s, ± 150°/s, ± 300°/s settings - Tri-axis accelerometer ± 10 g measurement.
Matt McKeever Jonathan Baker UAV Design Team 11/16/2006
Reegan Worobec & David Sloan In collaboration with UAARG.
IO Controller Module Arbitrates IO from the CCP Physically separable from CCP –Can be used as independent data logger or used in future projects. Implemented.
MSD Project Configurable Control Platform for Unmanned Vehicles Project Review Joe Pinzone Alex Mykyta Roberto Stolfa Robert Ghilduta Jason Stanislawski.
Hardware Connections for DAQ- FPGA Interface Interface for Driver / Data Acquisition Board P09311 David Howe.
Slide 1UCSB CMS Weekly Status MeetingCMS 4-Hybrid Test System Sam Burke EE UCSB 4-Hybrid Thermal Test System Status 10 June Sam Burke UCSB HEP Group.
Lesson 16: Aircraft Instrument Systems
Pressure Sensors Absolute – A Sensor That Measures Input Pressure in Relation to a Zero Pressure. We Will Use the Absolute Pressure Sensor to Calculate.
Measuring Pressure. Atmospheric Pressure Recall: Caused by the weight of the air molecules above us. Typically kPa or Pa Measured using.
Team Members Jordan Bennett Kyle Schultz Min Jae Lee Kevin Yeh.
Prof. Kristofer S.J. Pister’s team Berkeley Sensor and Actuator Center University of California, Berkeley.
Computer-Based Instrumentation 11/12/01 ISAT 300.
LSU 06/04/2007Expanding the BASIC Stamp1 Expanding the BASIC Stamp: Useful peripherals Programming Unit, Lecture 6.
MSD Project Configurable Control Platform for Unmanned Vehicles Detailed Design Review Joe Pinzone Alex Mykyta Roberto Stolfa Robert Ghilduta Jason.
o Portable low-cost aerial drone that can be used for reconnaissance o Relay real-time video and data, like location, heading, battery life o Take high-resolution.
Justin Kenny – IME  Project Description + Goals  Block Diagram + Descriptions  Schematic + Layout  Construction, Testing + Problems.
OPENSOURCE UAV DEVELOPMENT BY FERİT ÇAKICI. Cost Platforms ^ $100,000,000s $1,000,000s $100,000s $10,000,000s $500s $10,000s.
ECE 477 Design Review Team 9  Fall 2009 Josh Piron, Jacob Pfister Kevin Templar, Mike Phillips,
HOPE Microelectronic Company website:
ELE22MIC Lecture 9 MULTIPLEXOR - DATA SELECTOR DEMULTIPLEXOR - DATA DISTRIBUTOR Parallel to Serial Data Conversion External Address Bus Latching Address.
Low Voltage Power Supplies I.Placement II.Size III.Power consumption IV.Cabling V.Regulators board blocs VI.Component selection VII.Schematics VIII.Firmware.
FE-I4 Test Setup Hardware Needs: Boards & Interfaces March 1 st 2010, Marlon Barbero.
Aerospace Digital Communication Instrument Senior Design 1 Presentation.
Team 18: Humble Hubble The proposed project is a self-aiming telescope. This telescope will interface with a host device to populate a list of celestial.
Interactively change status, schedules, setpoints and strategies
Humble Hubble Team 18 Tim Brown. Abstract The proposed project is a self-aiming telescope. This telescope will obtain its global position and the local.
Search Pilot Qualification Course Civil Air Patrol Auxiliary of the United States Air Force.
Aerospace Digital Communication Instrument Senior Design Presentation.
Built-In Test Software for Deformable Mirror High Voltage Drivers Built-In Test Software for Deformable Mirror High Voltage Drivers Jianwei Zhou Home Institution:
Design Constraint Presentation Team 5: Sports Telemetry Device.
Three Factors of Weather
o Portable low-cost aerial drone that can be used for reconnaissance o Relay real-time video and data, like location, heading, battery life o Take high-resolution.
Robert Harris. Abstract What is "Hackers of Catron"? o Electronic Settlers of Catan® board. Settlers of Catan is a resource gathering and trading board.
Prepared by: Careene McCallum-Rodney Multiplexor.
Powered Flight Syllabus #4 CAP O-Rides Squadron 85.
Fundamental Digital Electronics
Team01: Zelun Tie The design project Wall-E Prototype I is an intelligent automated trash collecting robot with obstacle detection capability. The robot.
Hardware Needs 18F452 Main Controller CM8870 DTMF Decoder UART in PIC, MAX232 Serial Port Line Level Converter Amplifier for IR Detector Voltage feed into.
ECET 340 Entire Course (All ilabs and Homework) For more classes visit ECET 340 Week 1 HomeWork 1 ECET 340 Week 1 iLab 1 ECET 340.
RYAN LIPSKI, CAMERON PUTZ, AND NICK SIKKEMA ADVISOR: DR. JOSEPH DRISCOLL DEPARTMENT OF ELECTRICAL AND COMPUTER ENGINEERING, BRADLEY UNIVERSITY NOVEMBER.
Zilogic Systems 1 Device Interfacing with Python and ZIO Zilogic Systems.
Cloud Cap Technologies
A. Aloisio, R. Giordano Univ. of Naples ‘Federico II’
Electronics: Technologies, Definitions and Introductory Concepts
Next Generation Calculator Measurements
Device Interfacing with Python and ZIO
SArduino Training 2018 cho THPT Saigon Institute of Technology
ADC, DAC, and Sensor Interfacing
GSM - GPS BASED VEHICLE TRACKING SYSTEM
Cypress PSoC 3 vs. TI UCD90160 Power Supervision Applications
ECET 340 Competitive Success/snaptutorial.com
ECET 340 Education for Service-- snaptutorial.com.
Behavior of Gases.
Controlling Sensors Efficiently with MCUs
EVLA MONITOR & CONTROL CDR
TEAM BRIGHTRIDERS Schematic and PCB.
Arduino Board.
Cessna Equipment.
George Hadley Kelli Hacker Sean Ma Jacob Champion
ADC and Sensor Programming
UNR Quad turbulence experiment on March-15, 2018 Set number : 5
Arduino Workshop University of Jordan.
Arduino Workshop University of Jordan.
The BalloonSat Development Board
96Boards 2x20 header Power 12V 3.3V DES0558_10 Block Diagram V0.1
Presentation transcript:

I/O Breakout Board

DEVICE LIST FOR UAV IOB Analog Devices IMU Tyco Electronics GPS Airspeed Differential Pressure Sensor Altimeter Absolute Pressure Sensor Thermistor

I/O Breakout Board Diff V_IN max. ( V+) - ( V-)+/- 3.1 V V_IN max.V+ or V-5.1 V V_IN min.V+ or V-- 0.1V TI ADS1178 SensorVout MaxVout MinV-Vref Airspeed Altitude Temperature V- Calculation Airspeed Sensor: (4.7V +.2V)/2 = 2.45V Altitude Sensor: ( 4.5V +.5V)/2 = 2.5V Temperature Sensor: (4.986V +.229V) / 2 = 2.493V Vref Calculation Airspeed Sensor: (4.7V -.2V)/2 = 2.25V Altitude Sensor: ( 4.5V -.5V)/2 = 2.0V Temperature Sensor: (4.986V -.229V) / 2 = 2.38V

I/O Breakout Board Digital Peripherals: Tyco Electronics GPS – UART (NMEA) Analog Devices IMU – SPI Telemetry (P10231) – I2C, SPI, UART

I/O Breakout Board MUX IC Manual Override: 2 – Quad 2 to 1 multiplexers

I/O Breakout Board Molex 24 position connector Standard DSUB Connectors Pitot-Static Probe (Airspeed) Ram Air Pressure Stagnation (Static)

Feedback: Privacy Policy Feedback
Do Not Sell My Personal Information
About project: SlidePlayer Terms of Service

© 2025 SlidePlayer.com. Inc. All rights reserved.