Dr. John R. Samson, Jr. Honeywell Defense & Space, Clearwater, FL Précis 14 th High Performance Embedded Computing Workshop 16 September 2010 Dependable.

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Presentation transcript:

Dr. John R. Samson, Jr. Honeywell Defense & Space, Clearwater, FL Précis 14 th High Performance Embedded Computing Workshop 16 September 2010 Dependable Multiprocessor (DM) Implementation for Nano-satellite and CubeSat Applications (Challenging Packaging for High Performance Embedded Computing)

2 Overview Space applications have been, and will continue to be, subject to severe size, weight, and power constraints The need for/use of high performance embedded computing in space exacerbates the size, weight, and power problems Flying high performance embedded computing in nano-satellite and CubeSat applications presents unique problems which require unique solutions Small, light-weight, low power, COTS Computer-on-Module (COM), e.g., Gumstix, technologies are potential solutions to the size, weight, and power problems Platform- and technology-independent Dependable Multiprocessor Middleware (DMM) allows COMs to be used in nano-satellite and Cubesat applications

3 P-POD After CubeSat Ejection ^ * Excerpted from “CubeSat: The Development and Launch Support Infrastructure for Eighteen Different Satellite Customers on One Launch,” Jordi Puig-Suari, Clark Turner, & Robert J. Twiggs, California Polytechnic University, 15th Annual Utah State University Conference on Small Satellites ^ Excerpted from Nanosatellite Separation Proposal, “Nanosatellite Separation Experiment Using a P-POD Deployment Mechanism,” John Sangree, the University of Texas at Austin, circa 2007 Size and Weight Challenges CubeSats are flown in various sizes - 1U and 3U CubeSats are the most popular - 6U and 12U CubeSats are on the drawing boards 1U and 3U CubeSats are launched from P-PODs (Poly-Picosatellite Orbital Deployers) A P-POD can launch three (3) 1U CubeSats, one (1) 1U and one (1) 2U CubeSat, or one (1) 3U CubeSat Prototype CubeSat Launcher and CubeSat Models * P-POD Launcher Launch Spring 1U CubeSat (10 cm x 10 cm x 10 cm)

4 Power Challenges – Generation & Dissipation Axial View of P-POD Launcher 3U CubeSat with Hinged Solar Panels Deployed 3U CubeSat with Hinged Solar Panels Folded Hinges Solar Panels 3U CubeSat with Hinged Solar Panels Partially Deployed 3U CubeSat with Hinged Solar Panels Fully Deployed Solar panels can be one- sided or two-sided Solar cells can also cover the sides of the CubeSat

5 Gumstix Cluster: Seven (7) Gumstix Modules on “Stage Coach” Expansion Board CubeSat Side ViewCubeSat Axial View Stage Coach Board 10 cm ~10 cm 10 cm BRE440 System Controller Ethernet Switch Gumstix Module Locations Fully populated board < 20 Watts Gumstix Processor Module: 58 mm (~2.28”) 17 mm (~0.67”) ~1600 DMIPS OMAP 3503 Application Processor with ARM Cortex -AP8 CPU 256 MBytes RAM 256 MBytes Flash Example: Gumstix™ Computer on Module (COM) - A Small, Light-Weight, Low-Power Processing Solution * * Using COTS parts Host Spacecraft Electronics (Power, Control, Attitude Determination, Communications) Host Spacecraft Electronics (Power, Control, Attitude Determination, Communications)