59th ANNUAL MEETING PROCEEDINGS (2003)
June 23-25, 2003
Hyatt Regency Hotel - Albuquerque, New Mexico
TABLE OF CONTENTS
PLENARY
SESSION
Protection of the U.S. Transportation Infrastructure that Relies on GPS
Michael E. Shaw, U.S. Department of Transportation, 1
Possibilities for a 27 Optimized Constellation
Karl Kovach, ARINC, 22
SESSION
A1: ADVANCED INTEGRATED GUIDANCE & NAVIGATION SYSTEM DESIGN
Use of Military GPS in a Civil Environment
D.A. Happel, Rockwell Collins, 57
Using the GPS/INS Generalized Evaluation Tool (GIGET) for the Comparison
of Loosely Coupled, Tightly Coupled and Ultra-Tightly Coupled Integrated Navigation
Systems
J.D. Gautier, B.W. Parkinson, Stanford University, 65
Results of Recent Testing of an Integrated GPS/WAAS/Loran Receiver
G.L. Roth, Locus, Inc.; J.H. Doty, P.Y. Hwang, Rockwell Collins, Inc.; M.J.
Narins, Federal Aviation Administration, 77
Initial Flight Test Result of the GPS/INS Integration System with Integrity
for a UAV (Unmanned Aerial Vehicle)
S.H. Oh, D.H. Hwang, S.J. Lee, Chungnam National University, Korea; S.H.
Kim, Navicom Co., Ltd., Korea, 104
SESSION
A2: MEMS NAVIGATION
Foot-to-Foot Range Measurement as an Aid to Personal Navigation
T.J. Brand, R.E. Phillips, Charles Stark Draper Laboratory, Inc., 113
A Personal Navigation System Using Low-Cost MEMS/GPS/Fluxgate
S.Y. Cho, K.W. Lee, Kwangwoon University, Korea; C.G. Park, J.G. Lee, Seoul
National University, Korea, 122
MEMS-Based IMU Development, Calibration and Testing for Autonomous MAV Navigation
S. Winkler, M. Buschmann, T. Kordes, H.-W. Schulz, P. Vörsmann, Technical
University of Braunschweig, Germany, 128
High Accuracy MEMS GPS/INS for Commercial Applications
T. Shiozawa, H. Kumagai, Tamagawa Seiki Co., Ltd., Japan, 135
SESSION
A3: ALGORITHMS AND METHODS
Unambiguous Tracker for GPS Binary-Offset-Carrier Signals
R.L. Fante, The MITRE Corporation, 141
A Design Technique to Remove the Correlation Ambiguity in Binary Offset Carrier
(BOC) Spread Spectrum Signals
P.W. Ward, Navward GPS Consulting, 146
Study of the Impact of False Lock Points in Subcarrier Modulated Ranging
Signals and Recommended Mitigation Approaches
V.S. Lin, P.A. Dafesh, A. Wu, The Aerospace Corporation; C.R. Cahn, Consultant
to The Aerospace Corporation, 156
A Generalized Multiple Model Adaptive Estimator for Parameter and State Estimation
C.D. Ormsby, J.F. Raquet, P.S. Maybeck, Air Force Institute of Technology,
166
Optimal Success/Error Rate and Its Calculation in Resolution of Integer Ambiguities
in Carrier Phase Positioning of Global Positioning System
(GPS) and Global Navigation Satellite System (GNSS)
K. Kondo, Fujitsu Limited, Japan, 176
Performance Analysis of Geodetic-Grade GPS Receivers Based on Zero Base-Line
Measurements
G.E. Vázquez, The Ohio State University, 188
SESSION
C1: URBAN & LAND NAVIGATION
Enhancement of a Tightly Coupled GPS/INS System for High Precision Attitude
Determination of Land Vehicles
J. Wendel, T. Obert, G.F. Trommer, University of Karlsruhe, Germany, 200
Accuracy and Reliability Improvement of Standalone High Sensitivity GPS Using
Map Matching Techniques
C. Basnayake, G. Lachapelle, University of Calgary, Canada, 209
SESSION
C2: MARITIME NAVIGATION
Ship GPS Multipath Detection Experiments
G. Lachapelle, O. Julien, G. MacGougan, M.E. Cannon, University of Calgary,
Canada; S. Ryan, Canadian Coast Guard, Canada, 217
A Demonstration of High Accuracy Loran-C for Harbor Entrance and Approach
Areas
P.F. Swaszek, University of Rhode Island; G. Johnson, C. Oates, John J.
McMullen Associates, Inc.; R. Hartnett, U.S. Coast Guard Academy; G. Weeks,
U.S. Coast Guard Loran Support Unit, 230
SESSION
C3: NOVEL NAVIGATION SYSTEM APPLICATIONS
MEMS Inertial Sensor Assembly for Vestibular Prosthesis
M.S. Weinberg, The Charles Stark Draper Laboratory, Inc.; C. Wall, III,
Mass. Eye and Ear Infirmary & Harvard Medical School, 240
GPS Corn Maze, A New Satellite Navigation Application
F. Boynton, Navtech GPS Supply, 250
GPS-Based 3D Navigation Visualization for High Altitude High Open Parachuting
B. Balazs, M. Miller, T. Jacobs, Air Force Institute of Technology, 255
An Innovative Low Cost Location Determination System for Railroad Positive
Train Control Applications
J.B. Archibald, T.J. Meyer, Lockheed Martin, NE&SS, Niagara Operations,
267
Augmenting Parachute Testing and Evaluation Using GPS-Based Position and
Velocity
C. Schutte, M. Miller, J. Raquet, Air Force Institute of Technology; R.
Tredway, Air Force Research Laboratory Munitions Directorate, 273
Navigation Using Optical Measurements of Objects at Unknown Locations
J. F. Raquet, M. Giebner, Air Force Institute of Technology, 282
SESSION
D1: MILITARY NAVIGATION
Results of Shipboard Relative GPS (SRGPS) Testing for the Pegasus X-47A Unmanned
Combat Air Vehicle (UCAV)
P. Sousa, L. Wellons, Naval Air Systems Command, 291
G-STARTM, Lockheed Martin's Advanced GPS Anti-Jam Technology
B. Haefner, J. Naylor, S. Sorber, Lockheed Martin Systems Integration, 301
SESSION
D2: AVIATION NAVIGATION
Synthetic Pressure Altitude: An Alternative Means to Achieve Reduced Vertical
Separation Minima Aviation Altimetry
G.A. McGraw, K. Reichenauer, P. Hwang, Rockwell Collins, 308
Modeling GPS Receiver Performance in Civil Aviation Trajectories Using Current
GPS Constellation Performance
P.A. Seward, M.L. Boggs, B.R. Larson, Naval Air Warfare Center Weapons Division
(NAWCWD), 317
SESSION
D3: GNSS INTERFERENCE
Characterization of Narrow-Band Interference Mitigation Performance versus Quantization
Error in Software Radios
C. Cutright, Ohio University; J.R. Burns, Federal Aviation Administration;
M.S. Braasch, Ohio University, 323
GPS Antenna Mask Ring (GAMR)
G. Graham, US Army Aviation Missile Command; J.W. Smith, CAS Inc., 333
The Effect of Interference Power and Bandwidth on Space-Time Adaptive Processing
T.D. Moore, Veridian Systems Division; I.J. Gupta, The Ohio State University,
337
SESSION
D4: SPECIAL TOPICS IN NAVIGATION
The Evaluation of Navigator's Heart Rate Variability in an Inland Sea
K. Murai, Y. Hayashi, M. Nishiyama, Kobe University of Mercantile Marine,
Japan, 347
Improvement of Modular Terrain Navigation Systems by Measurement Decorrelation
J. Metzger, G.F. Trommer, University of Karlsruhe, Germany, 353
GPS Carrier-Phase Multipath Model Validation
S.K. Kalyanaraman, M.S. Braasch, Ohio University, 363
The Role of a Bluetooth-Equipped GPS Receiver in Intelligent Transportation
Systems
D.N. Aloi, Oakland University; L. Fay, M. Ronning, M. Willer, Sony Semiconductor,
372
A Simple and Effective Instantaneous Method for Initial Spacecraft Attitude
Estimation Using GPS Phase Difference Measurements only
R. Sánchez-Maestro, S. de Miguel-Sanz, SENER Ingeniería y
Sistemas S.A., Spain, 379
SESSION
E1: SURVEYING, GEODESY, & MAPPING
Kinematic Carrier Phase GPS Positioning Aided by an Instantaneous Local Ionospheric
Model Based on Multiple Base Stations Using Kriging
Y. Yi, D.A. Grejner-Brzezinska, The Ohio State University, 387
Network Approach to Precise GPS Navigation
P. Wielgosz, The Ohio State University and University of Warmia and Mazury
in Olsztyn, Poland; D. Grejner-Brzezinska, The Ohio State University; I. Kashani,
Israel Institute of Technology, 397
Deriving Vehicle Topology and Attribute Information Over Transportation Corridors
From LIDAR Data
D. Grejner-Brzezinska, C. Toth, The Ohio State University, 404
SESSION
E2: SPACECRAFT NAVIGATION & ATTITUDE DETERMINATION
On-Orbit Validation of GPS IIR Autonomous Navigation
J.A. Rajan, M. Orr, P. Wang, ITT Industries, 411
Space Navigation with Digital Beam Steering GPS Receiver Technology
K. Gold, R. Silva, R. Worrell, A. Brown, NAVSYS Corporation, 420
Navigation Services of the Mars Network
T.A. Ely, J. Guinn, E. Quintanilla, Jet Propulsion Laboratory, California
Institute
of Technology, 427
SESSION
E3: ADVANCED NAVIGATION SYSTEM TESTING (COMPONENT & SYSTEM LEVEL)
The Use of Optimal Smoothing and Nonlinear Filtering in Pseudolite-Based Positioning
Systems
T.J. Bouska, J.F. Raquet, P.S. Maybeck, Air Force Institute of Technology,
435
Development of an Expendable Real-Time GPS-Based Time-Space-Position Information
(TSPI) System Using COTS Hardware
J.A. Rogers, M.L. Boggs, B.D. Scott, B.M. Hoem, Naval Air Warfare Center
Weapons Division (NAWCWD), 444
Analysis of Range Safety Boundary for Spacelift Range Link Analysis
J.C. Chen, C.C. Wang, D.A. Taggart, J. Yoh, Y.Y. Krikorian, N.N. Elyashar,
M.M. Cutler, The Aerospace Corporation, 449
Analysis of Flight Technical Error on Straight, Final Approach Segments
B.S. Levy, The MITRE Corporation; P. Som, R. Greenhaw, Federal Aviation
Administration, 456
Measuring Inertial Navigation System Responses to Sinusoidal Inputs
T.J. Kim, M.L. Pedroncelli, R.J. Morris, A.M. Petney, Sandia National Laboratories
468
SESSION
E4: EARTH & SPACE-BASED AUGMENTATION SYSTEMS
Availability Enhancements for CAT IIIB LAAS
C.A. Shively, T.T. Hsiao, The MITRE Corporation, 474
LAAS Ranging Error Overbound for Non-Zero Mean and Non-Gaussian Multipath
Error Distributions
I. Sayim, B. Pervan, Illinois Institute of Technology, 490
LAAS Reference Antennas - Circular Polarization Mitigates Multipath Effects
A.R. Lopez, ARL Associates, 500
SBAS L1/L5 Signal Design Options
M. Tran, C. Hegarty, The MITRE Corporation; A.J. Van Dierendonck, AJ Systems;
T. Morrissey, Zeta Associates, 507
DGPS Accuracy Observations and Potential Data Channel Improvements
R. Hartnett, K. Gross, B. Bovee, S. Nassar, U.S. Coast Guard Academy; G.
Johnson, G. Sanders, John J. McMullen Associates, Inc.; P. Swaszek, University
of Rhode Island; D. Wolfe, U.S.C.G. Command and Control Center, 518
The Rosum Television Positioning Technology
M. Rabinowitz, J.J. Spilker, Rosum Corporation, 528
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