Antenna Performance Metrics for GNSS
Transcription
Antenna Performance Metrics for GNSS
Antennas for GNSS Applications Maged Shenouda Date: February 19, 2015 Agenda GNSS Constellations Antenna Performance Metrics for GNSS Antennas for GNSS Applications Positioning Studies Study 1 – Rooftop Survey Study 2 – PPP Position Accuracy using L-band delivered Corrections Study 3 – ALIGN Heading Application Summary NovAtel Inc - Proprietary NovAtel Inc. Proprietary GNSS Constellations Constellation Band Operation Bands (MHz) GPS L1 1563 - 1587 L2 1215 - 1240 L5 1164 - 1188 L1 1593 - 1610 L2 1238 - 1254 L3 1190 – 1214 E1 1563 - 1587 E5a/b 1164 – 1188, 1195 - 1219 E6 1267 - 1291 B1 1560 - 1591 B2 1167 - 1217 L-Band 1525 - 1560 GLONASS Galileo BeiDou Various NovAtel Inc - Proprietary NovAtel Inc. Proprietary Owner Various GNSS Bandwidths drive Antenna Bandwidth Requirements Broadband antennas with excellent GNSS performance are desired New local GNSS systems going online: QZSS, INRSS - Antenna Performance Metrics for GNSS Parameter Definition Frequency GNSS frequencies received Phase Center Offset (PCO) Antennas electrical center Phase Centre Variation (PCV) Variation of PCO over azimuth Multipath Rejection Ability to reject GNSS reflections Axial Ratio How well antenna is Right Hand Circularly Polarized (RHCP) Polarization Shape traced by E-field vector Gain Gain at zenith (90°) referenced to isotropic antenna Gain Roll-off Gain reduction from zenith to horizon All of these metrics impact position accuracy! NovAtel Inc - Proprietary NovAtel Inc. Proprietary Key Antenna Parameters vs. Application Survey GIS Reference Station Aviation/ Aerial Survey Marine Construction/ Mining Precision Agriculture Vehicle Tracking Dock Operations Unmanned Aircraft Unmanned Vehicle Timing Application Single Frequency ● ● ● Multi-Frequency (RTK) ● ● ● ● ● ● ● ● ● ● ● ● ● ● ● ● ● ● High Multipath Rejection ● ● ● ● ● ● ● ● ● ● Gain ● ● ● ● ● ● ● ● ● ● ● Gain Roll-off (Low elevation gain) ● ● Axial Ratio ● ● ● ● ● ● ● ● ● ● Ultra-low PCO/PCV ● ● Low PCO/PCV ● ● ● ● ● ● L-band frequency (Correction Services) Narrow Bandwidth (interference rejection) All of these metrics impact position accuracy! NovAtel Inc - Proprietary NovAtel Inc. Proprietary ● ● Antenna Performance Metrics for GNSS Polarization describes shape drawn by E-field vector as a wave propagates through space RHCP: Right Hand Circular Polarized LHCP: Left Hand Circular Polarized RHCP Wave (Source:http://en.wikipedia.org/wiki/Circular_polarization) NovAtel Inc - Proprietary NovAtel Inc. Proprietary Antenna Performance Metrics for GNSS What’s the most important parameter for a GNSS application? » Many in GNSS assume gain most important » Actually, it depends on the application » Examples: • Environment with heavy cover (such as forest) ! multipath rejection and gain are most important • Precision Survey: PCO most important, gain still matters but not as much • Mobile GPS: gain, PCO, PCV, etc. have less importance as accuracy goal is +/- 5m NovAtel Inc - Proprietary NovAtel Inc. Proprietary Antennas For GNSS Applications Antenna Type Low-cost single-feed Patch • Smaller Size; PCB Printed • Narrowband, poor AR and MPR • Poor low elevation tracking Multiple-feed Patch Euclidean Spiral (Pinwheel) Helix Choke Ring AntiJamming Typical Characteristics • Small Size; PCB Printed • Improved AR and MPR • Improved low elevation tracking • Supports all GNSS Bands • Excellent gain at multiple frequencies • Stable phase centers • Good AR and MPR • Highly circular polarized (good AR) • Stable PCO, low gain roll-off • Larger size needed for good gain • Excellent gain, PCO, MPR • Good low elevation tracking • Large size and weight • Array of several elements • Contains electronics, firmware, and/or beam forming to mitigate jamming sources • High cost and design complexity NovAtel Inc - Proprietary NovAtel Inc. Proprietary Examples Study #1 – Rooftop Survey » 3 NovAtel FlexPak6 receivers each connected to: • One GPS L1 only low cost single-feed patch antenna • One GPS/GLONASS L1/L2 multiple-feed patch antenna • One Pinwheel L1/L2 Antenna Purpose: Demonstrate how antenna selection affects position NovAtel Inc - Proprietary NovAtel Inc. Proprietary Study #1 – Rooftop Survey Antenna Type Gain Gain Roll-off PCO PCV Multipath Rejection Axial Ratio Pinwheel Antenna ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ GPS L1 Only Single Feed Patch ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ ★ GPS L1/L2/L5 Multi-feed Patch ★ ★ Legend ★ ★ ★ = Excellent ★ ★ = Good ★= Fair NovAtel Inc - Proprietary NovAtel Inc. Proprietary Measured C/No (dB-Hz) Study #1 – Rooftop Survey C/No is good but varies between antenna types NovAtel Inc - Proprietary NovAtel Inc. Proprietary Study #1 – Rooftop Survey Trajectory Plots Pinwheel GPS L1 Patch Pinwheel • • Tight cluster of points Additional bandwidth aids solution L1/L2/L5 Patch GPS L1 single-feed Patch • • • Largest distribution despite gain rivaling Pinwheel Only one band supported Poor PCO, PCV, MPR, AR limit accuracy of solution NovAtel Inc - Proprietary NovAtel Inc. Proprietary L1/L2/L5 multi-feed Patch • • • Larger distribution of points Much lower gain than pinwheel Roll-off, PCO, PCV, MPR aid accuracy of solution Study #2 – Position Accuracy with PPP Corrections » Study demonstrates how choice of antenna can impact Precise Point Position (PPP) accuracy and convergence time using corrections delivered via L-band » Pinwheel vs. Multi-feed patch – Pinwheel yields reduced position error and faster convergence time Antenna is an important consideration Horizontal Position Errors (Clear Sky) using L-band correction service NovAtel Inc - Proprietary NovAtel Inc. Proprietary Study #3 – Heading Application » Use NovAtel ALIGN algorithm to generate a GNSS based heading solution • Used to determine heading on moving and stationary vehicles and structures • Uses a master and rover antenna on same vehicle or structure • Relative heading and pitch computed with respect to a master antenna and receiver Study: Difference in heading accuracy using different antennas (Pinwheel vs. L1/L2 multi-feed patch) NovAtel Inc - Proprietary NovAtel Inc. Proprietary Rover Antenn a Master Antenna Study #3 – Heading Application » Assess heading performance using matched antenna types on various baselines 200 cm • 200 cm baseline – Typical for many heading applications 20 cm • 20 cm baseline – Approaching shortest baseline possible with Pinwheel antenna due to enclosure size Purpose: Demonstrate how antenna selection affects position Baseline distance between Master and Rover antennas NovAtel Inc - Proprietary NovAtel Inc. Proprietary Study #3 – Heading Application » Test jig installed in an open sky area • Stationary for entire proof of concept test » Collected 6-8 hours of 1Hz ALIGN data » Heading error with a small patch antenna is 3X greater than when using pinwheel technology » Choice of antenna in the application affects the heading error NovAtel Inc - Proprietary NovAtel Inc. Proprietary Summary GNSS Antenna characterized by several metrics: gain, gain roll-off, multipath rejection, axial ratio, bandwidth, PCO, PCV. Gain is not necessarily the most important metric. Antenna selection has an impact on all GNSS applications to varying degrees, needs to be carefully evaluated for a particular application! Survey, PPP positioning using L-band delivered corrections, and Heading applications are shown to be impacted by antenna selection. A well-designed antenna is a critical part of a GNSS System. NovAtel Inc - Proprietary NovAtel Inc. Proprietary Centimeter Positioning with a Smartphone-Quality GNSS Antenna Ken Pesyna, Todd Humphreys and Robert Heath The University of Texas at Austin Radiosense, LLC Motivation “I predict that by the GPS World dinner in 2020, carrierphase differential GNSS, will be cheap and pervasive. We’ll have it on our cell phones and our tablets. There will be app families devoted to decimeter- and centimeter-level accuracy…This will be the commoditization of centimeterlevel GNSS.” –Todd Humphreys, GPS World Dinner 2012 Focus Our focus has been on single-frequency carrier-phase differential GPS/RTK techniques. Why? 1. Our smartphones have single-frequency antennas 2. As compared to PPP, CDGPS/RTK has faster convergence times 3. Reference stations will eventually proliferate, making dual-frequency less important 4. Single-frequency Antennas are cheap! $0.02 (smartphone) - $5 (low-quality patch) The Primary Challenge: Awful Antennas Antenna Axial Ratio Polarization Loss in Gain compared to Surveygrade Survey-grade 1 dB @ 45° RHCP 0 dB High-quality Patch 2 dB @ 45° RHCP 0 – 0.5 dB Low-quality Patch 3 dB (average) RHCP 0.6 dB Smartphonegrade 10+ dB Linear 11 dB Test Platform Clock Antenna Front-end Smartphone GNSS Chipset Filter LNA Data Storage GRID SDR Outputs: • Phase/ pseudorange measurements • Complex (I,Q) accumulations GRID SDR RTK Engine RTK Filter Outputs: • Cm-Accurate Position • Phase Residuals • Theoretical Integer Resolution Success Bounds • Empirical Integer Resolution Success Rates Gain Compared to a Geodetic-Grade Antenna (dB) Gain Compared to a Geodetic-Grade Antenna (dB) December 2014: Successful RTK positioning solution with a smartphone Handheld RTK result with some signals passing through user’s body GNSS “light painting” with a smartphone Residuals Comparison Standard Deviation: 3.4 mm Residuals Comparison Standard Deviation: 4.6 mm Residuals Comparison Standard Deviation: 5.5 mm Residuals Comparison Standard Deviation: 11.4 mm Residuals Comparison Standard Deviation: 8.6 mm Time to ambiguity resolution for static antennas Time to ambiguity resolution for static antennas Overcoming multipath with more signals A Mitigation Suited for Smartphones: Multipath suppression via receiver motion (1 of 2) Phase Residuals (No Motion) Phase Residuals (Motion) Residual Autocorrelation (No Motion) Residual Autocorrelation (Motion) A Mitigation Suited for Smartphones: Multipath suppression via receiver motion (2 of 2) radionavlab.ae.utexas.edu 13 The information contained herein is confidential and proprietary to Maxtena Inc. 4-02 L1/L2 Dual-Band Antenna Multiband Multifilar Antennas • High polarization purity • Very versatile design • Very compact All dimensions are in mm. The information contained herein is confidential and proprietary to Maxtena Inc. Features The M1227HCT-A2-SMA is Maxtena’s latest high performance active rugged antenna designed for L1/L2 GPS and GLONASS bands for GNSS satellite applications. Features • • • • • • • • • • L1/L2 GPS-GLONASS bands Rugged IP-67 rating Superior out-of-band rejection 50 V/m jamming resistant Very low noise figure SMA mount Ground plane independent GIS & RTK applications Regulated voltage Ultra light weight - 24 grams (typical) All dimensions are in mm. The information contained herein is confidential and proprietary to Maxtena Inc. Applications (1) Applications • • • • • • • • • • Precision navigation Precision timing Military & security Asset tracking Oil & gas industries Navigation devices Mining equipment LBS & M2M applications Handheld devices Law enforcement The antenna is designed for applications requiring greater accuracy than what L1 only antennas can provide. The information contained herein is confidential and proprietary to Maxtena Inc. Applications (2) Ideal for GIS & RTK applications • L1/L2 high performances • Superior out-of-band rejection • 50 V/m jamming resistant • Very low noise figure Ideal for UAV applications • Ultra light weight The information contained herein is confidential and proprietary to Maxtena Inc. Out of Band Rejection Superior out-of-band rejection A built in dual-stage-LNA and filtering offers up to 30dB gain (50 V/m jamming resistant) for GNSS applications that utilize both GLONASS and GPS. The information contained herein is confidential and proprietary to Maxtena Inc. 90 80 70 60 50 40 30 20 10 0 GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz Group Delay L1 GPS/ GLONASS 2.5 V 3 V 3.3 V 0 GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz GHz 31.8 mm 1.215 1.217 1.219 1.221 1.223 1.225 1.227 1.229 1.231 1.233 1.235 1.237 1.239 1.241 1.243 1.245 1.247 1.249 1.560 1.563 1.566 1.569 1.572 1.575 1.578 1.581 1.584 1.587 1.590 1.593 1.596 1.599 1.602 1.605 1.608 Phase Center Phase center is located along axis of symmetry of the antenna The information contained herein is confidential and proprietary to Maxtena Inc. 34.2 mm Group Delay L2 GPS/GLONASS 120 100 80 60 2.5 V 40 3 V 20 3.3 V Applications in Satellite M2M and Voice M1600HCT12-U.Fl M1590HCT22-SMA The information contained herein is confidential and proprietary to Maxtena Inc. Applications in Satellite M2M and Voice M1600HCT12-U.Fl M1590HCT22-SMA The information contained herein is confidential and proprietary to Maxtena Inc. The information contained herein is confidential and proprietary to Maxtena Inc.