Sonobuoy Position Location using the Military P(Y) Code

Similar documents
Operational Field Trials of GPS Equipped Sonobuoys

Low Frequency Coherent Source Sonobuoy

Test Results from a Precise Positioning and Attitude Determination System for Microsatellites using a Software-Defined Radio

Precise Positioning and Attitude Determination of Microsatellites using a Software-Defined Radio

A Modular Re-programmable Digital Receiver Architecture

CDMA Principle and Measurement

Integrating SAASM GPS and Inertial Navigation: What to Know

Implementing a GPS Waveform under the Software Communications Architecture

2009 CubeSat Developer s Workshop San Luis Obispo, CA

Miniaturized GPS Antenna Array Technology and Predicted Anti-Jam Performance

Underwater Acoustic Communication and Modem-Based Navigation Aids

Acoustic Communications and Navigation for Mobile Under-Ice Sensors

Ultra Electronics Integrated Sonar Suite

Test Results from a Digital P(Y) Code Beamsteering Receiver for Multipath Minimization Alison Brown and Neil Gerein, NAVSYS Corporation

BENEFITS OF A SPACE-BASED AUGMENTATION SYSTEM FOR EARLY IMPLEMENTATION OF GPS MODERNIZATION SIGNALS

IMPLEMENTING A GPS WAVEFORM UNDER THE SOFTWARE COMMUNICATION ARCHITECTURE

Future GNSS: Improved Signals and Constellations

Using GPS in Embedded Applications Pascal Stang Stanford University - EE281 November 28, 2000

Remote Sensing using Bistatic GPS and a Digital Beam Steering Receiver

Integrated GPS/TOA Navigation using a Positioning and Communication Software Defined Radio

High Gain Advanced GPS Receiver

The Case for Recording IF Data for GNSS Signal Forensic Analysis Using a SDR

GPS TSPI for Ultra High Dynamics. Use of GPS L1/L2/L5 Signals for TSPI UNCLASSIFIED. ITEA Test Instrumentation Workshop, May 15 th 18 th 2012

TEST RESULTS OF A HIGH GAIN ADVANCED GPS RECEIVER

HIGH GAIN ADVANCED GPS RECEIVER

Implementation and Performance Evaluation of a Fast Relocation Method in a GPS/SINS/CSAC Integrated Navigation System Hardware Prototype

Practical Use of Reconfigurable Radios in Air Combat Training Systems

TEST RESULTS OF A DIGITAL BEAMFORMING GPS RECEIVER FOR MOBILE APPLICATIONS

Security of Global Navigation Satellite Systems (GNSS) GPS Fundamentals GPS Signal Spoofing Attack Spoofing Detection Techniques

Satellite Navigation Principle and performance of GPS receivers

Open Source Software Defined Radio Platform for GNSS Recording, Simulation and Tracking

Intro to GNSS & Teseo-LIV3F Module for IoT Positioning

Multipath Mitigation Algorithm Results using TOA Beacons for Integrated Indoor Navigation

Test Results from a Novel Passive Bistatic GPS Radar Using a Phased Sensor Array

ASR-2300 Multichannel SDR Module for PNT and Mobile communications. Dr. Michael B. Mathews Loctronix, Corporation

t =1 Transmitter #2 Figure 1-1 One Way Ranging Schematic

A GENERAL SYSTEM DESIGN & IMPLEMENTATION OF SOFTWARE DEFINED RADIO SYSTEM

RF7020D13 13dBm ISM RF Transceiver Module V2.12

DYNAMICALLY RECONFIGURABLE SOFTWARE DEFINED RADIO FOR GNSS APPLICATIONS

2009 Small Satellite Conference Logan, Utah

0.6 kbits/s, the modulation shall be aviation binary phase shift keying (A-BPSK).

Single Chip High Performance low Power RF Transceiver (Narrow band solution)

A Software GPS Receiver Application for Embedding in Software Definable Radios

KINEMATIC TEST RESULTS OF A MINIATURIZED GPS ANTENNA ARRAY WITH DIGITAL BEAMSTEERING ELECTRONICS

Test Results of a 7-Element Small Controlled Reception Pattern Antenna

Wireless Medium Access Control and CDMA-based Communication Lesson 14 CDMA2000

RF4432 wireless transceiver module

RDT&E BUDGET ITEM JUSTIFICATION SHEET (R-2 Exhibit)

Mobile & Wireless Networking. Lecture 2: Wireless Transmission (2/2)

GPS/QZSS Signal Authentication Concept

UNIT 1 - introduction to GPS

Test Range Spectrum Management with LTE-A

L50 GPS Module Presentation

Q20 High Sensitivity GPS Integration Board. Specification. QinetiQ Proprietary. QinetiQ Proprietary QINETIQ/VENTURES/CV/SPEC070049/1A.

GPS Adjacent Band Compatibility Assessment

RSU-101E Specifica on

Riza Muhida. Presented at he 22nd Session of the Asia Pacific Regional Space Agency Forum (APRSAF 22), Bali, Indonesia, December 1 4, 2015

Jager UAVs to Locate GPS Interference

Satellite Communications Testing

Unmanned Air Systems. Naval Unmanned Combat. Precision Navigation for Critical Operations. DEFENSE Precision Navigation

Case Study: and Test Wireless Receivers

Blair. Ballard. MIT Adviser: Art Baggeroer. WHOI Adviser: James Preisig. Ballard

CH 4. Air Interface of the IS-95A CDMA System

POWERGPS : A New Family of High Precision GPS Products

Benefits and Limitations of New GNSS Signal Designs. Dr. A. J. Van Dierendonck AJ Systems, USA November 18, 2014

Update on GPS L1C Signal Modernization. Tom Stansell Aerospace Consultant GPS Wing

Future Concepts for Galileo SAR & Ground Segment. Executive summary

IMPLEMENTATION OF SOFTWARE-BASED 2X2 MIMO LTE BASE STATION SYSTEM USING GPU

An Introduction to Software Radio

First Measurements of Ionospheric TEC and GPS Scintillations from an Unmanned Marine Vehicle

SA-320 Installation Guide SA-320. Installation Guide. Date: Nov., 2004 Version: 1.0. All Rights Reserved

Catalogue

UNCLASSIFIED. R-1 ITEM NOMENCLATURE PE F: NAVSTAR Global Positioning System User Equipment Space

SwiftBroadband Technical workshop

Preliminary Results from a GPS-Based Portable Impact Location System 1

EFFECT OF PPD TYPE JAMMERS ON AVIATION GPS RECEIVERS

SNIOT702 Specification. Version number:v 1.0.1

Exploring Trends in Technology and Testing in Satellite Communications

Receiver Technology CRESCENT OEM WHITE PAPER AMY DEWIS JENNIFER COLPITTS

GPS Glossary Written by Carl Carter SiRF Technology 2005

GMS-5 Telemetry and Command SubSystem 1

The FEI-Zyfer Family of Modular, GPS-Aided Time & Frequency Systems

PLC2 FPGA Days Software Defined Radio

Wide Area Wireless Networked Navigators

LR1276 Module Datasheet V1.0

DESIGN AND PERFORMANCE OF A SATELLITE TT&C RECEIVER CARD

Foreword by Glen Gibbons About this book Acknowledgments List of abbreviations and acronyms List of definitions

TRANSMISSION OF RADIOMETER DATA FROM THE SYNCHRONOUS METEOROLOGICAL SATELLITE

USB Port Medium Power Wireless Module SV653

Introduction to Global Navigation Satellite System (GNSS) Signal Structure

Wireless Communication in Embedded System. Prof. Prabhat Ranjan

LoRa1278 Wireless Transceiver Module

Embedded Radio Data Transceiver SV611

GPS Module AGP3363. Product Datasheet & Design Guide <V1.0>

SA-320 Installation Guide SA-320. Installation Guide. Date: Mar, 2011 Version: 2.5. All Rights Reserved

LoRa1276 Catalogue

120W UHF Transmitter/Repeater

FieldGenius Technical Notes GPS Differential Corrections

ECE 476/ECE 501C/CS Wireless Communication Systems Winter Lecture 9: Multiple Access, GSM, and IS-95

Development of Ultimate Seamless Positioning System for Global Cellular Phone Platform based on QZSS IMES

Transcription:

Sonobuoy Position Location using the Military P(Y) Code 2005 Joint Undersea Warfare Technology Spring Conference March 30, 2005 Dr. Alison Brown NAVSYS Corporation Phone: 719-481-4877 email: abrown@navsys.com www.navsys.com Jim Lackemacher Sparton Electronics Phone: (386) 740-5315 email: jlackemacher@sparton.com www.sparton.com 1

What is the Problem Sonobuoys could benefit from precise GPS location to improve operations Improve accuracy and reduce aircraft vulnerability Allows networked sonobuoy positioning and stand-off operation OSD policy requires use of secure P(Y) code for GPS military applications C/A code GPS can be easily spoofed or denied in a tactical environment Current military GPS UE (SAASM) are too expensive for sonobuoy operation Conventional GPS solutions do not operate well in the challenging sonobuoy environment High degree of masking due to antenna s low elevation above the sea surface Long Time-To-First-Fix when coming out of storage. TTFF is also aggravated by high sea-states and/or high winds (up to hours!) RF interference from 1 watt of power adjacent to antenna 2

Alternative GPS Architecture OEM GPS Receiver RF/IF Correlators CPU RF Telemetry & multiplexer TCXO TIDGET Sensor Almanac and last position is stored in nonvolatile memory LAT, LON (Pseudorange) RF/IF Digital Data Buffer RF Telemetry & multiplexer TCXO TIDGET DATA PACKET TIDGET allows use of commercial GPS chips on buoy with secure P(Y) code signal processing performed in aircraft Client/Server architecture facilitates operation in high seastates and challenging sonobouy environment 3

P(Y) TIDGET Sonobuoy System Architecture RF Chip DSP TIDGET Data Data Storage GPS Sonobuoy Sensor RF Input from aircraft DIFAR antenna TIDGET Processing Station RF Input from aircraft GPS antenna GPS Receiver (existing) GPS Sonobuoy Sensor Channel select and geolocation data I/O FSK Uplink DIFAR Processing Station (existing) Aircraft Equipment 4

Desired GPS Sonobuoy Performance Position accuracy of < 100 meters Position refresh rate of < 3 minutes per buoy Uplink data link rate of 1200 bps DIFAR SSQ-53-F Buoy Weight : 18.9 lb. Length: 36.0 C.G. From Bottom: 14.8 NAWC-AD funded an SBIR to build and test 5 prototype GPS DIFAR sonobuoys 5

P(Y) TIDGET Sonobuoy Design Sparton DIFAR Sonobuoy and Acoustic Processor. Integrated P(Y) TIDGET sensor Modified with GPS uplink data. Design is backwards compatible with the existing DIFAR aircraft acoustic processor. TIDGET P(Y) Code Sensor mounted in the buoy float bag Power supply regulation and switching Low-cost P(Y) compatible RF front-end with integrated GPS patch antenna. TIDGET data buffer and state-control functions Sparton-designed GFSK (Gaussian Frequency Shift Keying) modulation circuit, outputting the modulation signal to the buoy electronics. 6

TIDGET assembly uses all Commercial Components TIDGET circuit board mounted in surface unit Includes GFSK modulation circuit 7

Q-53F Buoy with TIDGET Card The weight and overall form factor of the Q-53F buoy with added GPS capability remain unchanged. The bare buoy weighs 18.6 lbs and the buoy with sonobuoy launch container (SLC) weighs 23.6 lbs..25 inch GPS/antenna PCB spacing shown 8

DIFAR Composite Spectrum Freq pilot Phase pilot db( composite( flog nlog )) Omni hydrophone Difar hydrophone GPS modulation 0 5000 1. 10 4 1.5. 10 4 2. 10 4 2.5. 10 4 3. 10 4 3.5. 10 4 4. 10 4 4.5. 10 4 n flog nlog, Nbins T GPS Modulation added as a 4800 Baud GFSK Pseudo-Random Bit Stream Does not affect existing Sono Data demodulation as above current channel pass-band 9

Telemetry Sequence State 1... RF telemetry ON... GPS OFF.SRAM idle... Preamble transmit Reset Address pointer NCorrBuff 64 bit period 13.3376mSec State 2... RF telemetry OFF... GPS ON... SRAM idle... Program Infineon registers.reset Address pointer NbuoyI2C 280 bit period 58.352mSec State 3.. RF telemetry OFF... GPS ON.SRAM snapshot fill 64 bit period 13.33mSec 32 bit period 6.6688mSec NbuoyGPSin Nbuoyresync State 4... RF telemetry ON... GPS OFF... SRAM read... Transmit GPS data 262144 bit period (32768 bytes) 54.63081secs NbuoyGPSTx State 1... RF telemetry ON... GPS OFF.SRAM idle... Preamble transmit.reset Address pointer C00C33C3FF03CFCC TELEMETRY RF OFF 33333333 Snapshot GPS data transmission Data rate = 40000000/8336 =4798.4644913 bps Snapshot = 6.55 msecs Frame Length = 262608 bit period = 54.7275seconds Telemetry uplink briefly gated off during GPS snapshot collection to avoid interference 24 bit periods C00C33C3FF03CFCC 10

Aircraft Processing Unit Sonobuoy Software Defined Radio Processing uses 3 Waveforms GPS Waveform GPS L1 P(Y) Code Includes PPS-SM Security Processor Provides GPS reference data Sonobuoy Telemetry Waveform Data Processing for GFSK demodulation Acquisition, Tracking, Data demodulation and Frame Sync TIDGET Processing Waveform P(Y) Correlation on TIDGET data Computes Sonobuoy navigation solution Sonobuoy Test-Bed used a Compact PCI Software Defined Radio (SDR) 1 ½ ATR Aviation SDR has now been purchased by NAVAIR 11

Software Defined Radio DIFAR/GPS Digital Front-End DIFAR HI DIFAR LO (155-175) MHz (135-155) MHz (60-80) MHz BPF BW=20MHz (60-80) MHz BPF BW=20MHz 40 MHz A/D Converter 40 MHz A/D Converter T O V I F Receives both GPS and DIFAR uplinked signals GPS L1 (1563.42-1587.42)MHz BPF CF=1575.42 MHz 1505.5 MHz (58-82) MHz BPF BW=24MHz 40 MHz A/D Converter B O A R D S DIFAR Channel selectable through software control 12

TIDGET Waveform Processing TIDGET data provided by Telemetry Waveform TIDGET Correlation generates pseudo-ranges Buoy Navigation computed using Kalman Filter SGPS GPS Satellite Track Ephem STIDGET P(Y) GCF TIDGET Correlation Buoy Navigation P(Y)-code (10.23Mbps) recorded by GPS Waveform Ephemeris data provided by GPS Waveform 13 lla_out

TIDGET Waveform Results C/A and P(Y) Correlations are computed for all visible satellites P(Y)+C/A correlation peaks used to detect which satellites can be tracked Sonobuoy mask angle and wave motion will cut-off some satellites C/A P(Y) P(Y)+C/A C/N0 (db-hz) for Channels 0 through 7 23.4448 17.3604 38.4201 41.7175 35.2154 15.8219 18.9964 44.1526 32.2919 30.8377 35.5640 39.2597 35.3738 32.2720 32.0136 41.4152 27.8612 25.9788 40.2327 43.6369 38.0287 28.8691 29.0887 45.9957 14

Channels where SV Signal Detected 15

Lab Test - Sonobuoy Navigation Data 16

Sea Trial at New Smyrna Beach, FL Five Buoys were deployed between 10:25 am to 5 pm on October 26, 2004 The sea state through the trial was 4-5 with a 6-8 foot swell After each buoy deployment the boat was allowed to drift several hundred meters downwind before being motored back into the buoy field. 17

Satellites Tracked during Sea Trials Satellites below 30 degrees in elevation were rarely tracked (Predicted mask angle was 18.5 degrees). The additional masking may be due to wave obscuration or the buoy may be sitting lower in the water than was assumed 18

Boat Tracks and Buoy Tracks (units in meters) Test successfully demonstrated Client/Server P(Y) code Sonobuoy operation in Sea State 4-5 using a Software Defined Radio for the GPS signal processing 19

GPS Sensor Trade Study Summary Sensor Type C/A GPS Engine SAASM Engine P(Y) TIDGET Provides PPS solution No Yes Yes Does not require Buoy No (Initialization No (Both keying and Yes Initialization pre-launch needed to reduce initialization needed) TTFF in high sea state) Data-Link bandwidth Low Low Medium (4800 bps) requirements Security requirements Estimated Cost Modifications to aircraft Not compliant with GPS Security policy for combat support <$150 (including telemetry uplink) Buoy initialization device required Security device is on Buoy - Must be zeroized prior to mission end $2800 (+ telemetry uplink) Buoy initialization device required None all security devices on aircraft <$180 (with telemetry uplink and in large volume production) Software Defined Radio required (could use JTRS on aircraft) 20

Conclusion P(Y) TIDGET provides low cost, secure solution for sonobuoy positioning using GPS SBIR project resulted in a design for embedding GPS sensor into existing DIFAR sonobuoys Software Defined Radio was used to perform DIFAR Telemetry, GPS and TIDGET processing Sea Trials have demonstrated capability to provide secure P(Y) code GPS positioning capability for sonobuoys in sea-state 4-5 Parts for additional sonobuoys have been purchased to allow for further sea-trials and operational evaluation NAWC-AD POC: Rich Sensenig, Pax River 21