On-Board Computer Subsystem David Stockhouse

Slides:



Advertisements
Similar presentations
Advanced Cubesat Imaging Payload Robert Urberger, Joseph Mayer, and Nathan Bossart ECE 490 – Senior Design I – Department of Electrical and Computer Engineering.
Advertisements

Advanced Cubesat Imaging Payload
Team MADD Michael Davies Andrew Mountain Dan Hoang Daniel Brink Team MADD Michael Davies Andrew Mountain Dan Hoang Daniel Brink Power Distribution Control.
Icarus Student Satellite Project Hannah Goldberg Dr. Brian Gilchrist BT Cesul Student Space System Fabrication Lab (S 3 FL) University of Michigan, College.
Auburn University Student Space Program. Overview of AUSSP Auburn University Student Space Program Made of two groups –Auburn High Altitude Balloon (AHAB)
Implementation of DSP Algorithm on SoC. Characterization presentation Student : Einat Tevel Supervisor : Isaschar Walter Accompany engineer : Emilia Burlak.
Payload Subsystem Integration and Testing Report Team Name 1 Team Name 2 Team Name N Universities/Institutions Team Members Date.
21st Annual Arizona Space Grant Consortium Symposium
Project ASCEND! Embry-Riddle Aeronautical University Spring 2014.
Continuing Embry- Riddle’s CubeSat Satellite Development Program Presented by Clayton G. Jacobs Embry-Riddle Aeronautical University, Prescott EagleSat.
33cm Band Communications for High Altitude Balloons Clayton G. Jacobs Tucson, Arizona April 21 st, 2012.
Memory Testing Payload for Nano- Satellite Matthew Vis Embry-Riddle Aeronautical University, EagleSat NASA Space Grant Intern Symposium, April 2015.
Project ASCEND! Embry-Riddle Aeronautical University Spring 2014 Presented By: Ankit Jain – Project Manager.
Development Progress of the EagleSat GPS Subsystem Presented by Tanner R. Hilken Embry-Riddle Aeronautical University, Prescott GPS Subsystem Lead.
GLAST LAT ProjectEGSE Peer Design Review, August 17, S. WilliamsEGSE Overview Electrical Ground Support Equipment Overview Scott Williams Stanford.
TRIO-CINEMA 1 UCB, 2/08/2010 Instrument Interface Board Dorothy Gordon CINEMA - EE Team Space Sciences Laboratory University of California, Berkeley.
Flight Testing Small Satellites Through High Altitude Ballooning Presented by Zach Henney 18 April 2015.
August 2003 At A Glance The IRC is a platform independent, extensible, and adaptive framework that provides robust, interactive, and distributed control.
Arizona Space Grant Symposium April 19, 2008 SWE Imaging Payload Command and Data Handling Jordan Cluster.
Designing a Communications System for Eagle Lisa Ferguson Dr. Gary Yale, Dr. Ed Post Arizona Statewide Symposium Announcements April 12, 2014.
Greg Alkire/Brian Smith 197 MAPLD An Ultra Low Power Reconfigurable Task Processor for Space Brian Smith, Greg Alkire – PicoDyne Inc. Wes Powell.
P08311: FPGA Based multi-purpose driver / data acquisition system Sponsor: Dr. Marcin Lukowiak Team MemberDisciplineRole Andrew FitzgeraldCEProject Manager/FPGA.
Space Grant Symposium, Apr USAF Academy’s FalconSAT-2 Program “Learning Space by Doing Space” C2C Eric Hutcheson Information Management NCO CS-25.
Slide 1 Shaun Houlihan Pumpkin, Inc. Applying Standard Commands for Programmable Instruments (SCPI) to CubeSats.
EagleSat-1 Continuing Embry-Riddle’s CubeSat Satellite Development Program
Real Time Systems Lab. 1 AV1394 Board : Now and Future Real Time Systems Lab. Myung Jin (Daniel), Lee.
Simplifying Customer Software Integration Tim Myers April 9 th, 2011 Colorado Undergraduate Space Research Symposium Payload Configuration GUI.
Arizona Space Grant Symposium
GLAST LAT ProjectSLAC Internal Review, April 16-18, 2002 LAT-PR Electronics and Flight Software WBS GLAST Large Area Telescope: Electronics,
CFS Use at Goddard The Johns Hopkins University Applied Physics Laboratory core Flight Software System Workshop October 26, 2015 Alan Cudmore – NASA Goddard.
SOIS Services. Layered View This is the traditional diagram that summarizes SOIS services in layers of a protocol stack.
Computer Memory Testing System for Nano-Satellite Matthew Demi Vis 1.
Freescale™ and the Freescale logo are trademarks of Freescale Semiconductor, Inc. All other product or service names are the property of their respective.
OBC Shawn Thompson Demi Vis 1. OBC Outline Requirements Concept of Operations Subsystem Description Development Environment/Tools Theory of Operations.
Kentucky Space Enterprise Missions
2. The main SDAQ functions 3. The description of the GAMMA-400 sDAQ
Simulation-to-Flight 1 Additional Resources:
USNA Standard CubeSat Bus USNA-P1 CubeSat (USNA-14)
Stefano Levorato INFN Trieste
Reconfigurable Computing for Space Applications
GLAST Large Area Telescope:
CFTP ( Configurable Fault Tolerant Processor )
Design of Two Payloads and NDVI Analysis on a High-Altitude Balloon
ENG3050 Embedded Reconfigurable Computing Systems
James Webb Space Telescope
Overview of Embedded SoC Systems
Electrical Ground Support Equipment Verification Test Support
Michael Fusco AZ / NASA Space Grant Scholar
EagleSat-1: Flight Operations
RECONFIGURABLE PROCESSING AND AVIONICS SYSTEMS
Project METEOR [P08102 RITSAT I]
EagleSat 2: Scientific Payloads’ Overview and Developments
EagleSat 2: Implementation of Improved Communications Systems on UHF Steven Buck Dr. Gary Yale, Embry-Riddle Aeronautical University Arizona Space Grant.
EagleSat 2: Design Development Lauren Barthenheier Dr
SLAC DOE Program Review
EagleSat 2 – Program Overview
EagleSat 2 – Scientific Payloads’ Objectives and Developments
EagleSat 2 – Electrical Power Subsystem Development
Pima Community College ASCEND Flight: Spring 2010 A post-mortem!!!
Eagle Space Flight Team Electronics Team
EagleSat-I Integration and Testing of 1U CubeSats
EagleSat 2: Design Development Lauren Barthenheier Dr
Mark Suder
TCP/IP Communications over Iridium Satellite Modems
Eagle Space Flight Team A Student Team’s Plan to Fly a Rocket to Space
AZ/NASA Space Grant Symposium
EagleSat 2 – Mission and Development Overview
<Your Team # > Your Team Name Here
Formula Electric Vehicle
We are working on developing “cheap” RTD monitoring channels for the CMS Phase-2 requirements. The channels will provide the complete readout for 4-wire.
Presentation transcript:

On-Board Computer Subsystem David Stockhouse EagleSat 2: On-Board Computer Subsystem David Stockhouse Arizona Space Grant Symposium April 14, 2018

Overview System-level description of satellite Computational needs for each subsystem On-board computer subsystem architecture In-depth look at payload prototypes Next Steps

System-Level Description

Computational Needs – Bus Systems Communications – Command reception and data transmission EPS – Power monitoring ACS – Attitude telemetry and control GPS – Position telemetry

Computational Needs – Payloads Cosmic Ray Payload (CRP) Interfacing with CMOS image sensor Image processing to determine energy and trajectory of particle events observed Memory Degradation Experiment (MDE) Interfacing with several SPI memory chips Identifying and characterizing memory errors

OBC Subsystem Architecture Two separate computer systems Payload Computer Interfaces to payload hardware and processes data Will be designed and built in-house based on Zynq-7000 SoC Command and Data Handling Computer Interfaces to other subsystems and status telemetry instruments Commercial off the shelf GOMSpace Nanomind A3200

Payload Prototype – CRP Developed on Avnet Zedboard Zynq-7000 contains both ARM processor system and FPGA programmable logic Xillybus interface between processor and FPGA Xillinux Linux distribution with application code on processor system FPGA design integrated with Xillybus IP Uses CMV2000 CMOS image sensor Breakout board designed in-house Complete system design and testing is ongoing

Payload Prototype – MDE Developed on Texas Instruments TM4C123GXL Memory board developed in-house Testing ongoing since February

Next Steps Miniaturizing CRP prototype High altitude balloon test flight Payload prototypes on fully custom PCBs More capable flight hardware

Acknowledgements Embry-Riddle College of Engineering NASA Space Grant Dr. Gary Yale – Faculty Supervisor Dr. Brian Davis Dr. Akhan Almagambetov

Thank You David Stockhouse EagleSat 2 On-Board Computer Lead stockhod@my.erau.edu Questions?

Backup Slide CRP Prototype Block Diagram