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长基线RTK实验

Long-baseline RTK-GPS/GNSS has the potential to enable positioning over distances of hundreds or thousands of kilometers. However, several error sources increase with baseline length, such as satellite ephemeris errors, ionospheric delays, and tropospheric delays. Achieving fast and reliable integer ambiguity resolution over long distances is challenging. Improving satellite orbit and clock information through use of precise ephemerides can help reduce some errors. Continued research on ambiguity resolution strategies is needed to enable practical long-baseline RTK positioning.

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0% found this document useful (0 votes)
50 views13 pages

长基线RTK实验

Long-baseline RTK-GPS/GNSS has the potential to enable positioning over distances of hundreds or thousands of kilometers. However, several error sources increase with baseline length, such as satellite ephemeris errors, ionospheric delays, and tropospheric delays. Achieving fast and reliable integer ambiguity resolution over long distances is challenging. Improving satellite orbit and clock information through use of precise ephemerides can help reduce some errors. Continued research on ambiguity resolution strategies is needed to enable practical long-baseline RTK positioning.

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wn1529.20000
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2009年度AOBセミナー

⻑基線RTK-GPS/GNSSの課題と展望
Overview of Long-Baseline RTK-GPS/GNSS

東京海洋大学 高須 知二

Long-Baseline RTK

2
RTK-GPS/GNSS
• Relative Positioning based on Carrier-Phase
– Real-time Position of A Moving Receiver
– Typical Accuracy: 1 cm + 1ppm x BL RMS (Horizontal)
– Transmit Reference Station Data to Rover via Wireless Link
– OTF (On-the-Fly) Integer Ambiguity Resolution
• Network-based RTK
– Single Receiver with Mobile Communication
– Commercial Services with Many Reference Stations
Reference Data Link Rover
Station Receiver

Applications of RTK-GPS/GNSS

Geodetic Survey Construction Precision Agriculture


Machine Control

ITS (Intelligent Mobile Mapping Sports


Transport System) System
http://www.trimble.com, http://www.leica-geosystems.com, http://www.gpsworld.com 4
Effect of Baseline Length
BL=0.3 km BL=13.3 km
RMS Error: RMS Error:
E: 0.2cm E: 2.2cm
N: 0.6cm N: 2.4cm
U: 1.0cm U: 10.6cm
Fix Ratio: Fix Ratio:
99.9% 94.2%

BL=32.2 km BL=60.9 km
RMS Error: RMS Error:
E: 10.0cm E: 14.0cm
N: 12.0cm N: 14.8cm
U: 30.2cm U: 26.7cm
Fix Ratio: Fix Ratio:
64.3% 44.4%

(24 hr Kinematic : Fixed Solution : Float Solution)


5

Demands of Long-baseline RTK


• No Reference Station in the vicinity of user
– Land of Vast Country (Russia, Canada, ...)
– Sea (Ships, Buy, Plants, Construction, …)
– Air (Flight), Space (Satellites)
• Need Separation of Movements between user
and reference
– Nation/World-wide Crustal Deformation Monitor
– Observation of Seismic Event by Large Earthquake

6
Long-BL RTK vs. Real-time PPP
Long-Baseline RTK Real-time PPP
Receiver Need Ref Station Single Receiver
Result Baseline Vector Position in Ref Frame
Baseline Length 100 km - 3,000 km Anywhere
Ephemeris Broadcast/Precise (IGU) Precise (IGU)
SV Clock Broadcast Precise (?)
Ionosphere Elimination/Estimation Iono-Free LC
Troposphere Model/Estimation Estimation
Antenna PCV Model Model
Earth Tides Ignored/Model Model/Estimated
Integer Ambiguity Fixed Float
7

Issues of Long-baseline RTK

8
Issues for Long-BL RTK
• Error Sources = Residuals of DD
– Satellite Ephemeris (BL=100 km- )
– Ionosphere (BL=10 km- )
– Troposphere (BL=50 km- )
– Antenna PCV, Earth Tides, Phase Windup ...
– Multipath + Receiver Noise (= Short BL)
• Strategy of Ambiguity Resolution
– Slow Convergence of Float Ambiguity Estimation
– Must Keep Integer Nature of Ambiguities
9

Broadcast Ephemeris
0.8 m

20,000
km

D.Boyd, GPS Constellation Status and Performance, CGSIC 49th, 2009


ΔrSD

ΔrSD = 0.8 m x 100 km/20,000 km = 4 mm 100 km


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Precise Ephemeris
IGS Product Table
Final Rapid Ultra-Rapid (IGU)
Broadcast
(IGS) (IGR) Observed Predicted

Orbit ~2.5cm ~2.5cm ~3cm ~5cm ~100cm

Accuracy ~150ps
~75ps RMS ~75ps RMS ~3ns RMS ~5ns RMS
Clock RMS
~20ps STD ~25ps STD ~1.5ns STD ~2.5ns STD
~50ps STD
17-41
Latency 12-18 days 3-9 hours realtime realtime
hours
every at 17 UTC at 03, 09, at 03, 09,
Updates -
Thursday daily 15, 21 UTC 15, 21 UTC

Orbit 15min 15min 15min 15min daily


Sample
Interval Sat: 30s
Clock 5min 15min 15min daily
Stn: 5min
(2009/8, http://igscb.jpl.nasa.gov/) 11

Improvement of IGU Orbit

(J. Ray et. al., Status of IGS Ultra-Rapid Products for Real-Time Applications, 2008 AGU Fall Meeting)
12
Accuracy of IGU-Predicted
PRN2

RMSE: R:0.8, A:3.5, C:2.8cm

PRN32

2009/5/27-31 RMSE: R:2.9, A:12.7, C:2.6cm


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Real-time Precise Ephemeris


• IGS RTWG+EUREF
• Orbit/Clock
– Orbit - IGU-Predicted
– Clock - Estimated
• Protocol/Format
– NTRIP v.1.0
– RTCM3 MT1057-1068
(Draft Proposal)

http://igs.bkg.bund.de/ntrip/orbits
14
Solar Cycle
International Sunspot Number (ISN): 1700-2009
20 21 22 23

by SIDC (Solar Influences Data Analysis Center) in Belglum (http://sidc.oma.be)

Solar Cycle Prediction: Cycle 24

23 24 24

by NOAA SWPC (Space Weather Prediction Center) (http://www.swpc.noaa.gov/SolarCycle)


15

Ionosphere Delay
SD L1 Vertical Ionospheric Delay (1 Week)
BL=100 km

RMS: 12.4 cm

BL=500 km

RMS: 30.8 cm
16
Tropospheric Delay
SD ZTD 2009/1/1-1/7 SD ZTD 2009/7/1-7/7
BL=100 km

BL=500 km

17

Integer Ambiguity Resolution (1)


• Ambiguity Resolution for Long Baseline RTK
– Eliminate Ionos with Integer Nature of Ambiguity
• Search Strategy for Short Baseline RTK
– Solve Statistically Optimal ILS Problem
– Efficient Strategy like LAMBDA
– Issue: No Ionos Elimination
• WL/NL Strategy for Static Post Processing
– Fix WL by Rounding of MW LC Average
– Fix NL by Rounding Iono-Free LC + WL
– Issue: Long Convergence, Reliability with Dual-Freq
18
Integer Ambiguity Resolution (2)
• RTKLIB v.2.3.0 (T. Takasu, 2009)
– EKF-based States Estimation
Rover Position, SD Vertical Ionos Delay, ZTD
Residuals for Rover/Ref, SD Float Ambiguity L1/L2
– Ionos: Random-Walk + Single Layer Model
– Tropos: A Priori Model + Random-Walk + NMF
– ILS Search by LAMBDA/MLAMBDA
– Partial Fixing with AR Elevation Mask
– Tight Constraint to Fixed Ambiguity (Fix and Hold)
19

Integer Ambiguity Resolution (3)


Full Fix
No Hold
(43.1%)

Partial Fix
No Hold
(86.2%)

Partial Fix
Fix and Hold
(96.8%)

v.2.3.1b, BL=100 km, 24 hr, Eph=IGS 20


RTKLIB

21

History
• 2006/4 v.0.0.0First version for RTK+C prog. lecture
• 2007/1 v.1.0.0Simple post processing AP
• 2008/7 v.2.1.0Add APs, support medium-range
• 2009/1 v.2.2.0Add real-time AP, support NTRIP,
start to distribute it as Open Source
• 2009/5 v.2.2.1 Support RTCM, NRTK, many receivers
• 2009/12 v.2.3.0 Support GLONASS, INS/GPS, …
• 2010/3? v.2.3.1 …
• 2010/5? V.2.4.0 Support Real-time PPP with IGS
22
RTKLIB APs
RTKNAVI, RTKRCV : Real-time positioning
RTKPOST, RNX2RTKP : Post-processing baseline analysis
RTKPLOT : Plot raw observation data and solutions
RTKCONV : RINEX converter for raw receiver log
...

23

RTKLIB v.2.3.1
• New Features
– Support Precise Ephemeris for Real-time AP
– Support Stream Type of FTP Download
– Tuning for Long-Baseline RTK
– Support Output Swap at day/hour boundary
– Improvement of Troposphere Model
– Full Positioning Options for RNX2RTKP
• Tuning for Long-Baseline RTK

24
Preliminary Evaluation (1)
BL 2009/1/1 - 1/7 2009/7/1 - 7/7
Rov Ref
(km) SDE SDN SDU Fixing SDE SDN SDU Fixing
3023 50.6 0.5 0.6 1.6 99.8% 1.6 1.9 5.7 90.2%
0586 100.2 0.7 0.9 2.5 98.7% 4.0 2.7 9.3 78.1%
0562 150.8 0.6 0.8 2.4 99.0% 3.7 2.2 6.6 83.6%
0241 200.4 0.7 0.9 2.2 99.5% 3.4 3.4 15.0 85.2%
0601 250.3 0.7 1.0 2.7 96.8% 3.2 2.1 6.5 79.1%
2110 0174 300.0 0.7 1.0 2.8 98.7% 2.0 1.8 5.2 88.0%
0579 351.9 0.9 0.9 2.8 99.3% 3.4 3.9 11.2 81.3%
0324 400.6 1.0 0.9 2.9 96.7% 2.6 2.0 6.5 74.3%
0905 450.6 3.2 5.4 21.2 64.8% 7.2 5.7 19.7 63.2%
0369 500.4 1.0 0.9 3.3 98.7% 2.4 1.8 6.0 85.6%
0837 995.6 3.1 1.9 8.5 91.4% 7.0 7.3 19.4 66.0%
SDE/SDN/SDU: Standard Dev E/N/U (cm), v.2.3.1b, Eph=IGS
25

Preliminary Evaluation (2)


2009/1/1-1/7 BL=100 km 2009/7/1-7/7

BL=300 km

26

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