MAXIM Data Systems Command & Data Handling Space - Ground Link Ground System 19 August 1999.

Slides:



Advertisements
Similar presentations
Satellite Communication
Advertisements

S. N. Satashia, Prem Kumar, M. Jeyamani & Tata Sudhakar
ECE 5233 Satellite Communications
All rights reserved © Altec ExoMars 2018 Rover Operations Control Centre Decision making process, Communications and Planning.
Page 1 Aalborg University Communication system for the AAUSAT-II Communication System for the AAUSAT-II Kresten K. Sørensen Department.
Alessandra Babuscia, Kar-Ming Cheung, Charles Lee, (Jet Propulsion Laboratory, California Institute of Technology) Mars CubeSat Workshop 20 th November2014.
Part2 course Network Planning and Link Budget Analysis 1.
Frank Stocklin Ron Vento Leslie Ambrose June 28,2001 SUPERNOVA/ACCELERATION PROBE (SNAP) Data Systems.
1 Transmission Media Lesson 04 NETS2150/ Lesson Outline Wired or guided Media –Electromagnetics waves are guided along a solid medium Wireless.
1 Satellite Link Equations Introduction to Space Systems and Spacecraft Design Space Systems Design.
Communications - Access Schemes 1 Introduction to Space Systems and Spacecraft Design Space Systems Design.
GROUP MEMBERS Jalil Ahmed Sadia Imtiaz Zaigham Abbas Faisal Jamil swedishcr.weebly.com 3.
Communication and Ground Station 12 October 2008.
Satellite Communication
Sistem Jaringan dan Komunikasi Data #3. Overview  guided - wire / optical fibre  unguided - wireless  characteristics and quality determined by medium.
G O D D A R D S P A C E F L I G H T C E N T E R 1 The Trade Between CCSDS and HDLC Framing on Global Precipitation Measurement David Everett and Jonathan.
VSOP-2 Ground Link Station - Tracking Station Requirements - National Astronomical Observatory of Japan Y. Kono.
ECEN 621, Prof. Xi Zhang ECEN “ Mobile Wireless Networking ” Course Materials: Papers, Reference Texts: Bertsekas/Gallager, Stuber, Stallings,
CSCI 465 Data Communications and Networks Lecture 6 Martin van Bommel CSCI 465 Data Communications and Networks 1.
Indian Ocean METOC Imager (IOMI) Operational Concept Demonstrates Military Operational Utility and Enables Improved Global Weather Prediction Data to Naval.
Sharif University of Technology Physical layer: Wireless Transmission.
NASA’s Goddard Space Flight Center LRO Operations Concept Richard Saylor Jr. HTSI/Code 444 August 16-17, 2005.
Student Satellite Project Tracking, Telemetry & Command UASat Progress Review Tracking, Telemetry and Command (TTC) January 26, 1999 Dana Irvin, Team Leader.
1 Titel van de presentatie Communications Communications architecture Frequency bands Ground-space link Intersatellite link Antenna configuration Tracking.
Autumn2004 © University of Surrey SatComms A - part 4 - B G Evans 4.1 Satellite Communications A Part 4 Access Schemes in Satellite Networks -Professor.
5 Section 11.0 Communications Subsystem Space Technology
1 How to design or select an antenna? Communications Crosslink scientific/housekeeping data (emitter & receiver sat) G/S link scientific data (emitter.
1 EE 499 Wireless Communications Project by Team 4: Arati NagarkarHemant Samtani Supriya HerwadkarChinmay Shete Shivani KaushalSalil Sawhney.
DINO PDR 17 October 2015 DINO Communication System Zach Allen Hosam Ghaith Mike Li.
Final Version Micro-Arcsecond Imaging Mission, Pathfinder (MAXIM-PF) Mission Operations Tim Rykowski Jeffrey Hosler May 13-17, 2002.
CCSDS P1A/B Meeting - Frascati - Nov 8, Gilles Moury, Guy Lesthievent - 1 Proposal to P1A & P1B Increasing allowed frame lengths and interleaving.
Section Number - 1 NASA’s Goddard Space Flight Center Communication Systems Jason A. Soloff NASA/GSFC Code 567 August 16-17, 2005.
1 The Global Positioning System (GPS). 2 nd USAF Space Operations Squadron.
Telecommunications AERSP 401B. Communication System Designers’ Goal Maximize information transfer Minimize errors/interference Minimize required power.
RF&Mod services from CIS-Lunar WG Single access? Multiple access? –To/from several s/c simultaneously from one station? (many to one) This might be useful.
SWE-DISH SATELLITE SYSTEMS
TRIO-CINEMA Meeting at KHU 1 October 19-23, 2009 CINEMA Operations Manfred Bester.
1 University of Maryland DYMAFLEX SHOT II Pre-Flight Presentation June 29, 2012.
AAE 450 – Senior Design J. Darcey Kuhn ERV Team – Communications January 23, 2001.
NASA’s Goddard Space Flight Center Lunar Reconnaissance Orbiter Ground System Requirements.
Final Version Frank Stocklin Ron Vento Bob Summers May Data Systems Micro-Arcsecond Imaging Mission, Pathfinder (MAXIM-PF)
The CCSDS Cislunar Communications Architecture Keith Scott The MITRE Corporation CCSDS Meeting January 2007.
NPOESS Transmission Frequency Issues Satellite Direct Readout Conference for the Americas 11 December 02 David F. McGinnis.
NASA MSFC Mission Operations Laboratory MSFC NASA MSFC Mission Operations Laboratory Ku - Band, DTN, and enhanced payload utilization.
Basic Satellite Communication (3) Components of Communications Satellite Dr. Joseph N. Pelton.
First Flight: Successful Use of a High Rate LDPC Code With High Data Rate in a Restricted Band H. Garon, V. Sank, W. Fong NASA/GSFC Spring Technical Meeting,
CINEMA PDR, UCB/SSL 1 August 22, 2008 CINEMA Communications & Ground Systems Manfred Bester.
AAE450 Senior Spacecraft Design Dorrie Byford Week 3: February 1 st, 2007 Communications Group Leader / Autonomous Rendezvous / Website and Database Designer.
From you host … Dr. H. Introduction Communications design requires us to think about the following issues: Communications design requires us to think.
Requirements to WSO Ground Segment Lavochkin Association & ROSCOSMOS 30/06/2006.
LuNet Integrated Network Architecture for Sustained Human and Robotic Exploration Gary Noreen Telecommunications Architect Communications Architecture.
IP Addressing & Routing - Down Downlink addressing –Normal addressing to any ground destination with normal ground routing –Packets addressed to another.
Spacecraft Systems Henry Heetderks Space Sciences Laboratory, UCB.
Low - Rate Information Transmission (LRIT) Downlink and Reception Satellite Direct Readout Conference for the Americas Frank Eng, Computer Sciences Corp.
From you host … Dr. H. Introduction In the present project, communications design forces us to think about the overall arrangement of the system and its.
Ground Control AERSP 401A. Ground System’s Basic Elements Mission Elements –Control the space segment or handle mission data, and includes: Ground Stations.
 From SmallSat to CubeSat: Reducing Mass Size and Cost Jeremy Straub 1, Ronald Fevig 2, Todd Borzych 2, Chris Church 2, Curt Holmer 2, Martin Hynes 2,
8.5 SATELLITE COMMUNICATIONS
Balloon Communications Kevin Shoemaker Shoemaker Labs, Inc. LCANS09.
Terry Smith June 28, 2001 Command and Data Handling System SuperNova / Acceleration Probe (SNAP)
TRIO-CINEMA 1 UCB, 2/08/2010 System Design Dave Curtis UCB/SSL Space Sciences Laboratory University of California, Berkeley.
Sketch for a telecoms system
FIXED SATELLITE SERVICE and UAS (22 September 2010)
USNA Next Generation Ground Station
H. Garon, V. Sank, W. Fong NASA/GSFC
SLS AREA REPORT Goal: Next Generation Uplink WG
Significant Milestones in Satellite Technology
ZERO LATENCY Satellite Data Delivery DEMAND AND CHALLENGES
EERF 6395 Navigation & Communication System for Deep Space Missions
Suggestion on your presentation of the TT&C subsystem
Presentation transcript:

MAXIM Data Systems Command & Data Handling Space - Ground Link Ground System 19 August 1999

MAXIM Data Systems Topics lData System Recommendations lOptions and Trades lSpectrum Utilization lGround Antenna Capabilities lData System Drivers lData System Block Diagram lMass/Power Summary lOperations Concept lLink Margin Summary lCost Data lSuggested Study Areas

Recommendations for MAXIM !Detector satellite will transmit science data using S-Band to Optics Spacecraft for combined transmission to ground stations !Store data continuously & dump daily for 12 min using DSN 34M using X-Band !Total downlink data rate: 300 Kbps !Use 2:1 data compression !Use S-band for Optics/Detector transmissions !Use S-band for backup comm from DSN for both Optics & Detector

Options/Trades !Detector spacecraft to transmit telemetry to Optics spacecraft for combined relay to ground station ( vs separate links) !Less ground station time required !Smaller antenna required for Detector Spacecraft & much simpler communication system !Optics spacecraft sends recorded data vs real time !Ground costs significantly less !Allows good availability on DSN 34M system

Options/Trades !DSN 34M recommended (vs 13M commercial) !Allows hi-rate playback !Reduces contact time !Much lower cost !Proven deep space operation !13 M commercial has unproven ranging capability at 40 million Km

Spectrum Utilization ØX-band Space to Ground Link Ø(+)Uplink and downlink frequency assignments available Ø(+) More efficient than S-Band (approx 11.5 dB) Ø(+)S/C hardware is available Ø(-) Rain attenuation (approx 2 dB) ØS-band for Optics/Detector link Ø(+ ) More efficient than X-Band (omni/omni) Ø(+) Existing hardware available with modifications of frequency Rx/Tx Ø(+) Allows backup to ground if needed (UHF not readily available) ØS-Band to ground link (emergency) Ø (0) Future allocation in DSN band may be questionable

Ground Antenna Capabilities DSN 34M: !X-Band Rx/Tx !G/T = 52.4 dBi/K !EIRP = 103 dBw max(can go to 110 dBw) !S-Band Rx/Tx !G/T = 42.1 dBi/K !EIRP = 98 dBw 13M commercial: ! X-Band Rx/Tx (uplink and ranging need to be added) !G/T = 37 dBi/K !EIRP = 90 dBw !S-Band Rx/Tx !G/T = 24.5 dBi/K !EIRP = 68 dBw

MAXIM Data System Drivers lMaximum Range: 40 million KM lDaily Data Volume: 432 Mbits

MAXIM Data Systems Block Diagram

RF Communications Mass/ Power Optics Spacecraft

RF Communications Mass/ Power Detector Spacecraft

DSN 34 M BWG (Stations at Canberra, Madrid, Goldstone) MAXIM MOC MAXIM Science Data MAXIM Operations Concept Diagram MAXIM Science X-band Kbps and Ranging S-band Emergency bps S-band command and 4 Kbps Telemetry (Housekeeping/Science) Commands S-band Emergency 12 bps and 100 bps

MAXIM Operations Concept !Detector spacecraft will continuously S-Band to Optics 4 Kbps (3 Kbps science, 1 Kbps housekeeping, uncompressed) !Optics spacecraft will compress 2:1 all Detector data and 1 Kbps Optics housekeeping data !Optics spacecraft will continuously record all compressed data for playback 1/day for Kbps to DSN X-Band through 1 of 2 HGA antennas !Nominal commanding/ranging to Optics spacecraft will be done via X-Band through DSN 34M BWG !Both Optics & Detector will have S-Band low-rate command/telemetry through DSN 34M for emergency operations !Commands throughput from MOC, telemetry FTP’d from fileserver

MAXIM Link Margin Summary All links have 3 dB required performance margins All links have rate 1/2 convolutional encoding

Cost Ground systems: !DSN 1hr/day = $365k/yr x 3= $1.1M !13M 8 hr/day = $7M Optics Spacecraft: !X Band !XPDRs (2) =$2M !HGA antennas(2)= $2M !S-band !XCVR(4) = $2.8M !omni antennas(4) = $300K !C&DH = $2M

Cost(cont’d) ØDetector Spacecraft: !S-band XCVR(2)= 1.4M !omni antennas(2) = $150K

Suggested Study Areas,Use of new coding schemes (e.g. Turbo Codes),Modified frequency scheme for S-band XCVR

Acronym List lACS - Attitude Control System lACU - Antenna Control Unit lBC - Bus Controller lBWG - Beam Wave Guide lDSN - Deep Space Network lFTP - File Transfer Protocol lHGA - High Gain Antenna lHSKP - housekeeping lI/F - Interface lMOC - Mission Operations Center lRF - Radio Frequency lSSR - Solid State Recorder lXCVR - Transceiver lXPDR - Transponder