Backup Trigger ANITA 2 SHORT boards are convert to full-band Modification: Break into the chain before the diode.

Slides:



Advertisements
Similar presentations
Controller Tests Stephen Kaye Controller Test Motivation Testing the controller before the next generation helps to shake out any remaining.
Advertisements

1 November NDIA Targets Symposium The Frequency Agile System  The Frequency Agile System Provides A New Concept for Naval Target Control:  Senses.
A 6 to 7 GHz front end for UWB based radio positioning
R. Mittra and A. Hoenschel EMC Lab, The Pennsylvania State University, University Park, USA Some Novel Designs for RFID Antennas and.
Team Impact Intelligent Helmet Impact System Critical Design Review February 28 th, 2008 Amanda Brodbeck Wei-Chu Liao Wei-Shen Liao Chris Mintle.
National Aeronautics and Space Administration — Balloon Program 2009 Bridging the Gap to Space The Micro-Instrumentation Package: A Solution for Lightweight.
1 Authored by John W. Desmarais Updated 10-Jun-2005 Modified by Lt Colonel Fred Blundell TX-129 Fort Worth Senior Squadron For Local Training Rev Jan-2014.
Team Flying Camels Nawar Chaker Pete Dokter Tim Jacobs Adam Swartley Paul Savage Capstone Project February 24, 2005.
Comments on this template -Leave time for questions -Leave time for demonstration (at the final LRR) -Use your actual hardware in the presentation -Practice.
Cornell University Space Systems Design Studio AIAA GNC Conference - 8/11/2009 Violet: A High-Agility Nanosatellite for Demonstrating Small Control-Moment.
Gary MKIII University of Central Florida Chris Valle, Braden Urban, John Rowe, and Tyler Yoemans.
16./ ANIMATE Telemetry Meeting ANIMATE Telemetry Meeting.
= Particle Astrophysics ANITA Collaboration Meeting UC-Irvine November 24-25, ANITA-lite: The Background Survey Jim Beatty Penn State.
UHM CanSat Team Members: Chris Ho: Team master, software Tyson Fukuyama: Hardware.
Aloha Proof Module Design Cabled Observatory Presentation School of Ocean and Earth Science and Technology February 2006.
STARLight PDR 3 Oct ‘01C.1 Hansen STARLight Peter Hansen PROJECT OVERVIEW.
Anita-lite UCLA-based Simulation Amy Connolly April 7 th, 2005.
EDGE™ MAV Control System - P09122 Final Project Review Erik Bellandi – Project Manager Ben Wager – Lead Engineer Garrett Argenna – Mechanical Engineering.
NAVO/PSI Buoy. Equipped with RTK GPS Rover Receiver, Buoy attitude and motion sensors, data acquisition system, and telemetry system. Reference Station.
COMM Subgroup Tomo Sugano (Primarily served as COMM personnel) Tasks –Started out by helping Relative Orbit team with differential delta-V requirement.
Preparations for GPS/INS Flight Testing on a High-Dynamic Vehicle Presenter: Curtis Cutright Advisor: Dr. Michael S. Braasch.
Flight Readiness Review Atomic Aggies. Final Launch Vehicle Dimensions Diameter 5.5” Overall length: inches Approximate Loaded Weight: lb.
Wireless Sea Measurement Unit A Plan for Aarne Halme Project Juha Vanhalakka Erkka Mutanen.
© Fraunhofer IIS GERMAN PARTICIPATION IN HF CHANNEL AVAILABILITY MEASUREMENTS Wideband Channel Availability Working Group –
Wind, wave and tidal energy DNV serving the energy industry.
B.E.E.P. Basic Earth Exploration Probe Siberian State Aerospace University Krasnoyarsk Russia International class.
VSOP-2 Ground Link Station - Tracking Station Requirements - National Astronomical Observatory of Japan Y. Kono.
Locate Wildlife Attach to Arrow Access Arrow Attach to Wildlife Does not alter Shot Detach from Arrow Link to Animal Remains attached during Flight Protect.
Active Target Multistatic Receiver (ATMR) John Paden.
Operational amplifier applications
+50dBm TX TPO: 100Watts (+50dBm) Start with a Transmitter.
Exercise. Try this A 100-Ω transmission line is connected to a load consisting of a 100-Ω resistor in series with a 10pF capacitor with 100Mhz signal.
John Clem and Paul Evenson University of Delaware 30-June-2010 Source of Funding/Grant : NASA Solar and Heliospheric Physics SR&T / NNX08BA62G AESOP Anti-Electron.
STARLight PDR 3 Oct ‘01 F.1.1 Rashid STARLight STARLight Mechanical Tahir Rashid STARLight Mechanical Engineer (734)
2.4 GHz CubeSat Communications System Robert Bui Communications Subsystem Lead.
Lecture 20: Communications Lecturers: Professor John Devlin Mr Robert Ross.
A PCB has 2 signal layers, a split power layer and one ground layer. It also has two solder mask and two silkscreen layers. Is the board classified as:
How much charge is in the battery. So we can keep the cars going for as long as possible and as fast as possible. To out find the aerodynamic and rolling.
Trimble NetR8 GNSS Reference Receiver
1 Blaster Analysis Update Peng Cao, John Clem, Brian Daily, Daniel DeMarco, Katie Mulrey and David Seckel Anita Meeting 12/May/2014.
ARISSat-1 Critical Design Review Orlando, Feb 15, 2010 U/v Transponder Bill Ress – N6GHz
LOS Downlink Systems Both systems are base upon commercial of the shelf technology.  900 MHz System based upon Freewave Technologies equipment.  2.4.
Running Piccolo Log on Flightgear Young Mo Kang UIUC.
AVAPS II DROPSONDE Overview
Group Five MSP430 Project Katy Charlton Jeremy McNutt Ben Ealey Aaron Vallance April 14, 2007.
FIELDS iCDR – RFS Analog Dennis Seitz 1 Solar Probe Plus FIELDS Instrument CDR RFS Analog Dennis N. Seitz UC Berkeley SSL
High-energy Electron Spectrum From PPB-BETS Experiment In Antarctica Kenji Yoshida 1, Shoji Torii 2 on behalf of the PPB-BETS collaboration 1 Shibaura.
University at Buffalo GLADOS SHOT II Balloon Launch Results Presentation July 1, 2012 Andrew Dianetti, Alex Wende, Bryant Carlson, Joe Flannery 1.
Doc.: IEEE /0112r2 Submission January, 2010 Hirokazu Sawada, Tohoku UniversitySlide 1 [Intra-cluster response model and parameter for channel.
FIELDS iPDR – RFS Analog Dennis N. Seitz 1 Solar Probe Plus FIELDS Instrument PDR Radio Frequency Spectrometer Analog Dennis N. Seitz UC Berkeley SSL
Notes on this template You may reformat this to fit your design, but make sure you cover the information requested in this template. Presentations should.
 ACCELEROMETER  TRANSMITTER- BLOCK DIAGRAM  RECEIVER- BLOCK DIAGRAM  COMPONENTS DESCRIPTION- ENCODER TRANSMITTER RECEIVER OPTICAL SENSOR.
Duplexer Repurposing Duplexer retired from Ely PD Originally tuned to TX RX MHz Frequency separation of 3.52 MHz Retune to Gilbert TX
OFDMA performance in 11ax
Fermilab 21cm Morocco Site Evaluation Status Kermit Carlson John Marriner Dave McGinnis Ralph Pasquinelli December 22, 2008.
OFDMA performance in 11ax
PROPELLER DISPLAY OF MESSAGE BY VIRTUAL LEDS
Implementation & Results
AC Inlet & AC Input Filter
Frequency Reconfigurable Microstrip Patch Antenna
Comparisons of Simultaneous Downlink Transmissions
VELO readout On detector electronics Off detector electronics to DAQ
HA1L High Altitude 1U Laboratory
Digital Sub-System Dorothy Gordon.
Sounding Rocket PDR Team Name
Sounding Rocket CDR Team Name
Antenna Design Tools VE3KL
OFDMA performance in 11ax
January, 2010 [Intra-cluster response model and parameter for channel modeling at 60GHz (Part 3)] Date: Authors: Hirokazu Sawada, Tohoku University.
<Your Team # > Your Team Name Here
Presentation transcript:

Backup Trigger ANITA 2 SHORT boards are convert to full-band Modification: Break into the chain before the diode

8 channels available per SHORT S11 measurements Completed ANITA 3 SHORT assembly

Iridium Open Port under evaluation as a possible Telemetry link Data Rates as high 80 kbps (observed during ground test) Data Transfer Bidirectional Frequency of Operation: TX and RX – 1616 to MHz at average power of 6 watts Photoshop Drawing for illustration (Drew Denny)

ANITA II Mast with flight GPS antenna mounted 4 GPS antenna Support Frame test setup (University of Delaware, Trabant Parking Structure, Top Level) University of Delaware

Altitude Check on the GPS signal simulator

New Flight Temperature Sensors are ready for integration

University of Delaware ANITA Campaign Personnel Primary Candidates: Katie Mulrey – Graduate Student John Clem – Scientist Secondary Candidate: James Roth - Senior Technician GSE Computer Support: Daniel DeMarco – Scientist / IT personnel