2003 NATIONAL TECHNICAL MEETING PROCEEDINGS
January 22-24, 2003
Disneyland Paradise Pier Hotel - Anaheim, California
TABLE OF CONTENTS
PLENARY
SESSION
GPtS, INtS and Critical Infrastructure
Prof. Bradford Parkinson, Stanford University, 1
WAAS Status
Leo Elderedge, Federal Aviation Administration, 24
LAAS Update
Gary Skillicorn, Federal Aviation Administration, 37
EGNOS
Dr. Javier Ventura-Traveset, European Space Agency, France, 51
Spectrum Interference
Sally Frodge, OST, U.S. Department of Transportation, 92
A1:
ALGORITHMS AND METHODS 1
Modeling Inertial Sensor Errors Using Autoregressive (AR) Models
S. Nassar, K-P. Schwarz, The University of Calgary, Canada; A. Noureldin, Royal
Military College of Canada; N. El-Sheimy, The University of Calgary, 116
Comparison of Solution Via Covariance Matrix and Convolution Integral for
INS Position and Velocity Errors Due to Deflections of Vertical
D. Hsu, Northrop Grumman, 126
An Efficient Computational Method for Horizontal/Vertical Exclusion Level
as Part of Fault Detection and Exclusion Implementation
L. Lupash, Trimble Navigation, Ltd, 133
Efficient Attitude Determination Algorithm Using Geometrical Concept: SNUGLAD
C. Kee, J. Jang, Y. Sohn, Seoul National University, Korea, 142
Development of an Alignment Process to be Used on Flight Tests Campaign of
a GPS Attitude Determination System
N. P. Oliveira Leite, Instituto de Aeronáutica e Espaço, Brazil;
F. Walter, Instituto Technológico de Aeronáutica, Brazil, 152
A2:
AUGMENTATION SYSTEMS: AVIATION 1
WAAS Observed Performance During 60 Day Test
T. McHugh, W. Wanner, Y-K. Vu, F. Lorge, Federal Aviation Administration; D.
Nelthropp, Titan Systems Corp., 163
WAAS Error Bounding During Ionospheric Storms
T.R. Schempp, L.J. Trautman, Raytheon Company, 175
Integrity Lessons from the WAAS Integrity Performance Panel (WIPP)
T. Walter, P. Enge, Stanford University; B. DeCleene, Federal Aviation Administration, 183
Possible WAAS Reference Station Locations in Alaska to Increase LPV Availability
E. Carolipio, H. Go, H. Wan, Raytheon Company, 195
Evaluating Candidate Algorithm and Architecture Improvements for the Next
Phase of WAAS
C. Griffith, H. Wan, H. Go, E. Carolipio, Raytheon Company, 203
Techniques for Graceful Reversion from Dual to Single Frequency WAAS
S-S. Jan, T. Walter, P. Enge, Stanford University, 214
A3:
SPACE APPLICATIONS
Modeling an Off-Nominal Launch Vehicle Trajectory for Range Safety Link Analysis
J.C. Chen, C.C. Wang, D. Taggart, E. Ditata, The Aerospace Corporation, 225
A4:
Interference and Spectrum Management
Radio Frequency
Interference Validation Testing for LAAS Using the Stanford Integrity Monitor
Testbed
M. Luo, G. Xie, D. Akos, S. Pullen, P. Enge, Stanford University, 233
B1:
ALGORITHMS AND METHODS 2
A New Approach to GPS Phase Multipath Mitigation
D. Bétaille, LCPC, France/University College London, UK; J. Maenpa, H.J.
Euler, Leica Geosystems, Switzerland; P. Cross, University College London, UK, 243
An Estimation Algorithm for Precision GPS Signal Monitoring
P.D. Groves, I.J. Richards, P. Briggs, QinetiQ Ltd., UK, 254
Precise Velocity Estimation Using a Stand-Alone GPS Receiver
F. van Graas, A. Soloviev, Ohio University, 262
An OFDM/FDMA Indoor Geolocation System
I.F. Progri, W. R. Michalson, D. Cyganski, Worcester Polytechnic Institute,
272
U.S. Coast Guard Integrated Navigation Systems
G.C. Hernandez, U.S. Coast Guard; J.F. Ryan, U.S. Merchant Marine, 282
B2:
AUGMENTATION SYSTEMS: AVIATION 2
Development of GRAS Cockpit Displays for Advanced Approach and Landing Procedures
W.S. Ely, Airservices Australia, Australia, 287
FAA Loran-C Propagation Studies
G.W. Johnson, JJMA, Inc.; R.J. Hartnett, U.S. Coast Guard Academy; P.F. Swaszek,
University of Rhode Island; K. Gross, U.S. Coast Guard Academy; C. Oates, JJMA,
Inc.; M.J. Narins, U.S. Federal Aviation Administration, 300
Experimental GBAS Performance at the Approach Phase
S. Saitoh, S. Fukushima, T. Yoshihara, N. Fujii, Electronic Navigation Research
Institute, Japan, 317
A Method for LAAS Fault-Free Error Overbounding Using a Position Domain Monitor
R. Braff, The MITRE Corporation, 326
Analysis of Vertical Alert Limit for LAAS CAT III Autoland
C.A. Shively, CAASD, The MITRE Corporation, 339
Loran Fault Trees for Required Navigation Performance 0.3
S. Lo, L. Boyce, T. Walter, P. Enge, Stanford University; B. Peterson, Peterson
Integrated Geopositioning; B. Wenzel, Booz Allen Hamilton; K. Carroll, USCG
LSU, 352
B3:
CARRIER PHASE BASED POSITIONING
Real-Time Kinematic Positioning Based on Un-Differenced Carrier Phase Data Processing
Y. Gao, K. Chen, X. Shen, University of Calgary, Canada, 362
Fast Ambiguity Resolution in RTK-GPS Positioning for Marine Navigation
F. Wu, N. Kubo, A. Yasuda, Tokyo University of Mercantile Marine, Japan, 369
The Use of Standardized Network RTK Messages in Rover Applications for Surveying
H.J. Euler, B.E. Zebhauser, Leica Geosystems AG, Switzerland, 377
Tightly-Coupled IMU/GPS Carrier-Phase Navigation System
J.F.M. Lorga, Q.P. Chu, J.A. Mulder, Delft University of Technology, The Netherlands, 385
Radar Altimeter Calibration of the Envisat Satellite: An Autonomous System
of High-Precision for Instantaneous Sea Surface Height Determination
T. Schueler, B. Zimmermann, B. Riedl, G.W. Hein, University FAF Munich, Germany, 397
Artificial Intelligence for Optimizing the GNSS Carrier Phase-Based Positioning
H.A. Saleh, IRIDIA, Université Libre de Bruxelles, Belgium, 407
C1:
MULTI-SENSOR INTEGRATED NAVIGATION SYSTEMS 1: HIGH PERFORMANCE APPLICATIONS
Analysis of Coast Times Upon Loss of GPS Signals for Integrated GPS/Inertial
Systems
Y.C. Lee, S. D. Ericson, The MITRE Corporation, 417
Adaptive Tightly-Coupled, a Low-Cost Alternative Anti-Jam INS/GPS Integration
Technique
P.D. Groves, D.C. Long, QinetiQ Ltd., UK, 429
Airborne Autonomous Fault Detection for Shipboard Landing Navigation Using
Carrier Phase DGPS
M-B. Heo, B. Pervan, Illinois Institute of Technology; S. Pullen, J. Gautier,
P. Enge, Stanford University; D. Gebre-Egziabher, University of Minnesota, 441
Quantifying Improvements from the Integration of GPS and a Tactical Grade
INS in High Accuracy Navigation Applications
M.G. Petovello, M.E. Cannon, G. Lachapelle, The University of Calgary, Canada,
454
MEMS Inertial on an RTK GPS Receiver: Integration Options and Test Results
T. Ford, J. Hamilton, M. Bobye, NovAtel Inc.; J.R. Morrison, B. Kolak, Honeywell
Inc., 466
F/A-22 Global Inertial Navigation System Certification Test Results
P.J. Thomas, ASC/YFFA (F/A-22 SPO); W. Powell, Lockheed Martin Aero Marietta;
D.L. Stutz, D. Craig, R. Lawrence, R.C. Sturdevant, 746th Test Squadron (CIGTF), 478
C2:
MODERNIZATION: GPS & GALILEO 1
GPS IIR-M: Modernizing the Signal-in-Space
J.A. Rajan, J.A. Tracy, ITT Industries, NJ Technology Center, 484
GPS Constellation Transition to Three Planes and Drifting Ground Tracks
J.H. Drake, Lockheed Martin Space and Strategic Missiles, 494
GPS III URA and URRA Information for Optimal User Performance
R. DiEsposti, J. DiLellio, D. Galvin, C. Kelley, J-M. Shih, The Boeing Company,
504
GPS Architecture Evaluations Based on Algorithmic Service Volume Model
K. Johnson, D. Diefes, Lockheed Martin Management and Data Systems, 513
Performance Evaluations of the New GPS L5 and L2 Civil (L2C) Signals
M. Tran, C. Hegarty, The MITRE Corporation, 521
GNSS II: Imperative for Galileo-GPS Rationalization and Harmonization
R.W. Skinner, Lockheed Martin Space Systems Company, 536
C3:
AUGMENTATION SYSTEMS: LAND & MARINE
Nationwide DGPS: 2003 and Beyond
D.B. Wolfe, C.L. Judy, A.B. Kritz, J.A. Chop, M. W. Parsons, USCG Command and
Control Engineering Center, 548
Demonstration of Decimeter-Level Real-Time Positioning of an Airborne Platform
M. Armatys, R. Muellerschoen, Y. Bar-Sever, R. Meyer, Jet Propulsion Laboratory,
California Institute of Technology, 558
A Global, High-Accuracy, Differential GPS System
R. Hatch, T. Sharpe, P. Galyean, NavCom Technology, Inc., 562
Status of the Loran Recapitilization Project (An Enhanced Vision of Loran)
G.K. Weeks, Jr., M. Campbell, K. Carroll, United States Coast Guard Loran Support
Unit, 574
Dynamic Evaluation of High Accuracy Differential GPS
M. Sergi, B. Newstrom, A. Gorjestani, C. Shankwitz, M. Donath, University of
Minnesota Twin Cities, 581
D1:
MULTI-SENSOR INTEGRATED NAVIGATION SYSTEMS 2: ALGORITHMS AND NOVEL APPLICATIONS
Navigating the Ground from Air: Active Monitoring with GPS/INS Geo-Referenced
LiDAR
A. Mohamed, Alberta Research Council, Canada, 593
Review of Potential Applications of Low-Cost GPS/INS for General Aviation
A. Soloviev, F. van Graas, Ohio University, 602
Performance Analysis and Architectures for INS-Aided GPS Tracking Loops
S. Alban, D.M. Akos, S.M. Rock, Stanford University; D. Gebre-Egziabher, University
of Minnesota, 611
Innovative Approach to Local Area Precise Positioning Using Direct Sequence
Spread Spectrum
D.W.A. Taylor, P.N. Johnson, ENSCO, Inc., 623
Assessment of Various Integrated Navigation Systems for the Toronto Transit
System
M. Abd El-Gelil, A. El-Rabbany, Ryerson University, Canada, 630
Adaptive Noise Reduction Model for MEMS-Based Inertial Sensors
M. El-Diasty, A. El-Rabbany, Ryerson University, Canada, 636
Thermal and Noise Characteristics of MEMS Inertial Sensors
W. Abdel-Hamid, N. El-Sheimy, G. Lachapelle, The University of Calgary, Canada,
641
D2:
MODERNIZATION: GPS & GALILEO 2
A Comparison of the Loss of Lock Threshold of BOC and NRZ Signals for First
Order Code Tracking Loops
J.K. Holmes, S.
Raghavan, The Aerospace Corporation, 649
Assessment of GEO Augmentation for GPS III Constellations
R.H. Clark, J.H. Drake, Lockheed Martin Space and Strategic Missiles, 657
Objectives of the Emerging WAAS L5 ICD and Goals of the Corresponding WAAS
L5 Signal
T.L McKendree, Raytheon Company, 663
Lessons Learned in the Certification of Integrity for a Satellite-Based Navigation
System
G.T. Watt, R.M. Fries, H.L. Habereder, D.R. Heine, T.L. McKendree, Raytheon
Company, 670
Defining the Elements of a Civil GPS Monitoring Service
J.W. Lavrakas, J.B. Broomfield, Overlook Systems Technologies, Inc., 683
GPS Integrity Failure Modes and Effects Analysis
K. Van Dyke, DOT/Volpe Center; K. Kovach, ARINC; J. Lavrakas, Overlook Systems
Technologies, Inc.; J.P. Fernow, MITRE CAASD; J. Carroll, J. Kraemer, DOT/VOLPE
Center; N. Attallah, B. Baevitz, SAIC, 689
D3:
INNOVATIVE APPLICATIONS
INS/DGPS Integration Utilizing Wavelet Multi-Resolution Analysis
A. Osman, The University of Calgary, Canada; A. Noureldin, Royal Military College
of Canada; S. Nassar, N. El-Sheimy, The University of Calgary, Canada, 704
GNSS Laboratory: Using the GPS as an Interdisciplinary Laboratory on Theory
of Telecommunications
D.R. Mendéz Castillo, F. Walter, Instituto Technológico de Aeronáutica
(ITA), Brazil; K.T. Fitzgibbon, EMBRAER, Brazil, 711
The Dependence of WAAS Ionospheric Error Bounds upon the Spatial Distribution
of GPS Measurements
L. Sparks, A. Komjathy, A.J. Mannucci, Jet Propulsion Laboratory, California
Institute of Technology, 719
Network Centric Mapping Database
W.J. Altice, R.P. Cooke, WR Systems, Ltd.; R.A. Greer, Space and Naval Warfare
Systems Center; Z. Yang, WR Systems, Ltd., 728
A Location Based Encryption Technique and Some of Its Applications
L. Scott, D.E. Denning, GeoCodex LLC, 734
Space Overlay for Homeland Security Communications and Navigation
L. Jocic, R. Buenneke, J. Fujita, The Aerospace Corporation; R. Ewart, G. Dildy,
D. Ballinger, M. Hobson, USAF Space and Missile Systems Center, 741
The Feasibility Study of Using GPS Buoy to Observe the Sea States in Hong
Kong
Y. Chen, W. Chen, D. Zheng, A. Chan, X. Ding, Department of Land Surveying and
Geoinformatics, Hong Kong Polytechnic University; J.C.H. Chao, Brilliant Technology
Development Ltd., Hong Kong, 748
E1:
RECEIVER AND ANTENNA TECHNOLOGY
Loran Aviation Receiver and RF Simulator Development
B. Peterson, K. Dykstra, Peterson Integrated Geopositioning, LLC, 755
A 12-Channel Real-Time GPS L1 Software Receiver
B.M. Ledvina, S.P. Powell, P.M. Kintner, M.L. Psiaki, Cornell University, 767
Characterization and Performance of a Prototype Wideband Airport Pseudolite
Multipath Limiting Antenna for the Local Area Augmentation System
J. Dickman, C. Bartone, Y. Zhang, Ohio University; B. Thornburg, dB Systems
Inc, 783
Flight Trials of a Novel Dual-Patch Anti-Jam GPS Antenna
F.N. Bauregger, T. Walter, D. Akos, P. Enge, Stanford University, 794
E2:
ATMOSPHERIC EFFECTS
Monitoring Space Weather with GPS Mapping Techniques
A. Coster, MIT Lincoln Laboratory; J. Foster, P. Erickson, MIT Haystack Observatory;
B. Sandel, Lunar and Planetary Laboratory; University of Arizona; F. Rich, AFRL,
800
4-D Modeling of Water Vapour Using a Regional GPS Network
S. Skone, S.M. Shrestha, The University of Calgary, Canada, 809
Tropospheric Delay Modelling for the European Space Agency's Galileo Testbed
Methods of Improvement and First Results
A. Pósfay, E. Krueger, T. Schueler, G.W. Hein, University FAF Munich,
Institute of Geodesy and Navigation, Germany, 817
Ionospheric Effect in Instantaneous Positioning
M. Gende, Universidad Nacional de la Plata, Argentina/Abdus Salam ICTP, Italy;
S.M. Radicella, B. Nava, Abdus Salam ICTP, Italy; C. Brunini, Universidad
Nacional de la Plata, Argentina, 826
Preliminary Evaluation of the Effects of Scintillation on L5 GPS and SBAS
Receivers Using a Frequency Domain Scintillation Model and Simulated and Analytical
Receiver Models
T. Kim, R.S. Conker, M.B. El-Arini, S.D. Ericson, C.J. Hegarty, M.Tran, CAASD/The
MITRE Corp., 833
Adapting Kriging to the WAAS MOPS Ionospheric Grid
J. Blanch, T. Walter, P. Enge, Stanford University, 848
Measurement Noise Versus Process Noise in Ionosphere Estimation for WAAS
J. Blanch, T. Walter, P. Enge, Stanford University, 854
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