IP For Responsive Microsats, A Practical Approach. Space Internet Workshop 5, 2006 Assi Friedman & Jeffrey Janicik Innoflight Inc.
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1 IP For Responsive Microsats, A Practical Approach Space Internet Workshop 5, 2006 Assi Friedman & Jeffrey Janicik Innoflight Inc.
2 Presentation Abstract Using Internet Protocols on smallsats started as a grass roots effort to take advantage of commercial hardware and software and save development time, money, and reduce risk. These premises are still exist today within the community.. In addition, even though the primary users of microsats nowadays are government customers (in the U.S.) the motivation for fast responsive microsats is consistent with the original premises. There are many spacecraft tracking stations available for government and commercial networks in the U.S. yet only few can support IP operations as a standard feature. Capitalizing on the benefits that IP can provide to us will come into play only if we can establish an operational baseline that is cost effective and easy y for spacecraft designers to implement. Using protocol on protocol or unique and proprietary encoding methods defeats the point as it is as efficient as designing your r own in-house system. Innoflight has been working on a number of microsat IP technology y solutions that will enable spacecraft builders to purchase COTS IP enabled hardware and software package for both the ground and flight segments. This presentation will describe how Innoflight integrated traditional IP/HDLC with CCSDS standards, and Type-1 encryption to provide users with secure, high performance IP link k between the spacecraft LAN and the ground segment
3 Who is Innoflight? The Innovative Implementation of COTS-Based Solutions for Affordable and Responsive Commercial and Aerospace Systems Communications Flight Hardware Small Sats Secure TCP/IP link engineering, integration, and hardware fabrication Analog (FM) and digital (GMSK/BPSK/ QPSK) RF engineering Experienced in VHF thru X-bandX Portable and fixed ground-based stations Miniature and non- traditional flight systems In-house concept-to to- product capability Skilled at low power, light weight designs and qualifying them for extreme environments High efficiency power systems Embedded systems On-board board-computers Controllers Command decoders High reliability supervisory circuits Experts in systems design, engineering, integration, test and operations Hands-on experience Network of vendors SEIT best practices for low-budget, quick- response programs
4 IP is an Enabler Ground Segment Motivation for Work Enables creation of virtual mission operations centers tied by private p and public IP networks Enables widest range of connectivity physical layers (Serial, Ethernet, PTP, Wireless, Dialup, ADSL, Cable, Satellite, etc ) Enables use of COTS platforms for user, and network hardware Space Segment Transforms C&DH and subsystems into a LAN of subsystem hosts Enables use of commercial and industrial IP stacks Overall System Reduce engineering time spent on transport and increases time put towards actual mission implementation
5 The Responsive Space Network IP in space is worthless if not implemented as a system!
6 On-Orbit Orbit Missions Practical IP implementation has been ad-hoc and non standard as any good evolutionary process is! DMC-UK HDLC based with SSTL style physical link encoding CHIPSat HDLC based with in-house link encoding Previous missions lack the powerful link characteristics of standard CCSDS encoding To the best of our knowledge IP over CCSDS hasn t been implemented and isn t t available commercially
7 A Practical Approach to IP Granted that HDLC is supported by most RTOS s and has been the focus of experimentation with IP in space CCSDC 131 offers powerful link encoding methods Bump in the wire approach allows combinations of powerful CCSDS standards with the reliability of commercial and industrial HDLC Bump in the Wire Subsystems RTOS with HDLC/IP CCSDS Link Modem Space Transceiver RF Users IP Router CCSDS Link Modem Ground Station
8 Ground IP Satellite Access System IPSAS-GND Data Encoder Randomizer Baseband Filter Ground Transceiver Uplink Modulator Data Encoder Derandomizer R-S Decoder Convolutional Decoder Downlink Demodulator Uplink No utility in FEC due to high link margins FEC processing on spacecraft is power consuming Data encoder NRZ/NRZI Randomizer CCSDS Baseband filter GMSK Raised Cosine Downlink QPSK With CCSDS convolutional decoder BPSK: no convolutional decoder Reed Solomon block decoder CCSDS Derandomizer CCSDS Data encoder NRZ/NRZI IPSAS = (Industry Standard TCP/IP) + (Aerospace Link Encoding)
9 Flight IP Satellite Access System HDLC formatted RS422 data in Data encoder PCM encoded serial bit stream Randomizer Randomized serial bit stream R-S encoder Reed- Solomon encoded bit stream Convolutional encoder Convolutional encoded I&Q bit stream to TX HDLC formatted RS422 data out Data decoder Derandomizer Bit sync Video or RS422 serial data from RX PCM encoded serial bit stream Randomized bit stream RS422 to C&DH Power input Command processor Power regulation Control of all IPSAS elements TX, RX, and internal power Telemetry Transmitter ADC Telemetry conversion & Control Transmitter telemetry & control Receiver telemetry & control TX RX
10 IPSAS-GND Prototype Router Interface RS232 Interface Ethernet Interface Transceiver Interface Control Processor Uplink FPGA Processor Power Regulation Downlink FPGA Processor
11 IPSAS Operational at USN IPSAS was deployed to USN in November 2005 System tested with Innoflight s s full spacecraft simulator IPSAS supports two operational on - orbit spacecraft Currently working on introducing support in additional ground station networks Radio IPSAS Router
12 TCP/IP Network Implementation w/usn RGS = Remote Ground Station NMC = Network Management Center Australia RGS Hawaii RGS Alaska RGS Secure Virtual Private Network tunnels (VPN s) between ground stations and NMC s INTERNET INTERNET Internet Users Prime Home Agent Backup Home Agent PA NMC CA NMC Slide source: IPCMS Project
13 Microsat Encryption Unit Bump in the wire approach allows additional relevant HQ C-7289, Phase 2 STTR with Missile Defense Agency TASK: Design and build an NSA certified, type-1 1 encryption device that is suitable for use on government microsats and supports TCP/IP communications protocols. Research Partner: Southwest Research Institute (SwRI) Gov t Assist: NSA Transceiver RED dashed: Plain text data BLACK dashed: Cipher text data BLACK solid: Control line BLUE solid: Operational (flight) power GREEN solid: Ground support programming power Radio Interface Key / Tunnel Programmer Crypto Device Key Loader Flash Memory Bus Interface Mode Controller Power Regulation C&DH Subsystem Bus RS422/485 Bus Power 10V-36V Key / Tunnel Load EGSE
14 Contact Information Assi Friedman Principal Engineer Tel: (858) ext. 13 Jeffrey Janicik CEO & President Tel: (858) ext. 12 Innoflight Inc Oberlin Dr. Suite 340 San Diego, CA Fax: (858) Questions anyone?
15 Backup Materials
16 IPSAS-GND Specifications Input Power Standard 110VAC Power < 10W Mechanical Form Factor Standard 19 rack, 2U height, 8 8 deep User Interface Remote configuration using Ethernet 10/100 Mbps TCP/IP Telnet (port 23) Simple ASCII protocol Local configuration RS232 Front panel aliveness status LED Non volatile memory for configuration storage Quality and Reliability Prototype Level First IPSAS-GND Prototype Under Test
17 IPSAS-GND Demonstration Specifications Downlink: Input: RS232 RS422 LVTTL Data & clock (invert capable) Data rate: up to10mbps Descrambler: ITU V35 / Intelsat CCSDS (modified) HAM Decoder: NRZ / NRZI FM0 / FM1 Output: RS232 RS422 LVTTL Data & Clock (invert capable) Uplink: Input: RS232 RS422 LVTTL Data & clock (invert capable) Data rate: up to100,000bps Encoder: NRZ / NRZI FM0 / FM1 Scrambler: Ham Radio CCSDS (modified) Output RS232 RS422 LVTTL Data & clock (invert capable) Analog GMSK 0.5 BT Raised cosine DC coupled
18 Analog Filter Options User Configured Two selectable analog out filters Data rate up to 100kbps 1.4 Vp-p into 50 Ohm load Gaussian, BT=0.5 (GMSK) Raised Cosine
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