PROCEEDINGS OF THE ION 57th ANNUAL MEETING Crowne Plaza Pyramid Hotel - Albuquerque, New Mexico TABLE OF CONTENTS PLENARY SESSION
GPS Modernization
D.
Loverro, U.S. Air Force, 1 GPS Interagency Forum for Operational Requirements
S.
Canzano, AFSPC/DRN, 33 Civil GPS Applications
M.E.
Shaw, U.S. Department of Transportation, 48 GALILEO: Project or Reality?
L.
Dutton, Thales Avionics, UK, 74 SESSION A1a: FUTURE GNSS MODERNIZATIONMeasurements of GPS Receiver Compatibility with Interplex-Modulated M-Code SignalsP.A. Dafesh, R.L. Wong, M.D. Partridge, T. Fan, The Aerospace Corporation, 100 Navigation Professionals' Public Policy Positions
on GLONASS G.C. Chachis, Titan Systems Corporation, 109 Matched Filter Mean Acquisition Time Performance
for P(Y), BOC(10,5), and MAN(10) Codes With FFT Aiding and Noncoherent
Combining J.K. Holmes, P.A. Dafesh, The Aerospace Corporation, 121 SESSION A1b: SPACE SYSTEMS & APPLICATIONS Feasibility of Managing a Dynamic Constellation
to a Fixed Constellation Definition B.P. Ayati, P.D. Massatt, The Aerospace Corporation, 140 Real-Time, Autonomous, Precise Orbit
Determination Using GPS D.B. Goldstein, U.S. Air Force, GPS Joint Program Office; G.H. Born, P. Axelrad, University of Colorado, 149 A Positioning System for GEO Satellites Using GOES Weather Satellites as GPS-Type Pseudolites R.B. Ward, L. Capots, Lockheed Martin Space Systems Company, 159 Tracking Loop Optimization for On-Board GPS
Navigation in High Earth Orbit (HEO) Missions J.L. Garrison, Purdue University; M.C. Moreau, P. Axelrad, University of Colorado, 168 SESSION B1: 150TH ANNIVERSARY OF THE GYROSCOPE: A HISTORICAL
PERSPECTIVE (IEEE Sponsored) History of Ring Laser Gyroscope Development at
Lockheed Martin (Formerly Sperry) J. Abdale, V. Benischek, W. Macek (retired), Lockheed Martin Naval Electronics and
Surveillance Systems, 176 No Moving Parts: A Fiber Optic Gyroscope R.W. Shorthill, University of Utah, 188 Evolution of Precision IFOG G. Adams, Honeywell International Corporation; N. Barnett, L. Insley, Penn State University Applied Research Laboratory; S. Vajda, Strategic Systems Program, 200 Aerospace Technology and Low Automotive Costs
Benefit Quartz Micromachined Gyros A.M. Madni, BEI Technologies, Inc.; L.E. Costlow, R.P. Jaffe, BEI Systron Donner Inertial Division, 205 Strategic Testing at the Central Inertial
Guidance Test Facility R.S. Lawrence, C.H. Barker, R.C. Sturdevant, 746th Test Squadron, 219 The History of Laser Gyro Development in the
Former Soviet Union D.P. Loukianov, Yu.V. Filatov, St. Petersburg State Electrotechnical
University, Russia;
V.N. Kuryatov, The Research and Development Institute
"Polyus", Russia; V.P.
Vasiliev, The
Institute for Precision Instruments Engineering, Russia; V.I. Buzanov, V.P. Spectorenko, O.I. Klochko, The Central Design Bureau and the Plant
"Arsenal", Russia, 225 SESSION C1: AVIATION APPLICATIONS Advanced Flight Display for General Aviation
Aircraft: A Cost-Effective Means to Enhance Safety J.G. Dubinsky, M.S. Braasch, M. Uijt de Haag, Ohio University Avionics Engineering Center, 238 Analysis of Differential Tropospheric Delay
Resulting from Vertical and Horizontal Displacements for the LAAS MOPS C. Varner, The MITRE Corporation, 247 LAAS Performance for Terminal Area Navigation R. Braff, The MITRE Corporation, 252 Antenna Techniques to Optimize Pseudorange
Measurements for Ground Based Ranging Sources J. Dickman, C.G. Bartone, Ohio University, 263 Aircraft Antenna Calibration for the LAAS VHF
Data Broadcast O.K. Nyhus, Honeywell; T.A.
Skidmore, A.A. Wilson, Ohio
University, 275 Integration of DGPS and Precision Tracking Radar
for Aircraft Precision Approach N. Nabaa, G. Clary, J. Cross, D. Howard, R. Thayer, Sierra Nevada Corporation, 284 SESSION D1: INTEGRATED POSITIONING & NAVIGATION SYSTEMS New Results from Time Domain Analysis of GPS
Jamming Interference J. Lukesh, Northrop-Grumman (retired), 291 Enhanced Precision Reference Systems R.S. Lawrence, R. Pearson, J. Sanchez, B. Neal, 746th Test Squadron; R. Gurr, Air Force Flight Test Center; N. Carlson, Integrity
Systems Inc., 304 Sensor Scheduling in Kalman Filters: Evaluating a
Procedure for Varying Submarine Navaids T.H. Kerr III, TeK Associates, 310 Pressure and Blanchard Altitudes Computed from
Atmospheric Data Gathered from May through July 2000 at White Sands, New Mexico T.-C. Li, D.N. Thunborg (retired), Northrop Grumman (Litton) Guidance & Control
Systems, 325 An Efficient Integration Scheme for the INS and
the Attitude Determination GPS Receiver S. Heon Oh, D.-H. Hwang, S. Jeong Lee, Chungnam National University, South Korea, 334 SESSION B2a: MARITIME NAVIGATION Support System for Economical Navigation in
Inland Seas by Using Current and Wind Information K. Murai, Y. Hayashi, Kobe University of Mercantile Marine, Japan, 341 LORAN-C Recapitalization Project (LRP) – Summer
2001 Update A.N. Arsenault, J.M. Boyer, United States Coast Guard, 346 A High Accuracy Hybrid Navigation System for
Unmanned Underwater Vehicle H. Kumagai, Ritsumeikan University/Tamagawa Seiki. Co., Ltd, Japan; M. Kihara, Y. Kubo, S. Sugimoto, Ritsumeikan University, Japan, 356 USCG Tender Deployable Differential Reference
Station D.B. Wolfe, D.J. Godfrey, R.W. James, United States Coast Guard Command and Control
Engineering Center, 364 Coverage Analysis of NDGPS Broadcast Sites D.B. Wolfe, D. Ojeda, D.J. Godfrey, J.L . Hartline, E.B.
Manley, United
States Coast Guard Command and Control Engineering Center, 370 SESSION B2b: ATMOSPHERIC EFFECTS ON NAVIGATION SYSTEMS Ionospheric Correction Improvements for Single
Frequency GPS Receivers A. Brown, A. Jovancevic, S. Ganguly, M. Kirchner, S.
Zigic, Center
for Remote Sensing, Inc., 376 Benefits of GPS Modernization to the Atmospheric
Science Community A.J. Van Dierendonck, AJ Systems; A.J.
Coster, MIT
Lincoln Laboratory, 382 Measuring Ionospheric Scintillation Effects from
GPS Signals A.J. Van Dierendonck, AJ Systems; Q. Hua,
GPS Silicon Valley, 391 SESSION C2: LAND, MOBILE, E911, TELECOMMUNICATIONS, & INTERNET APPLICATIONS OF GPS A Low Cost and Simple Approach for Driver
Navigation H. Agnew, V. Geake, C. Beatty, Yeoman Group plc, England, 397 Low-Cost Automotive Navigation Alternatives D.N. Aloi, J. Stefan, OnStar, 402 SESSION D2: ALGORITHMS AND METHODS FOR NAVIGATION SYSTEMS Real-time Minimization of the Total Tracking
Error in Phase and Delay Lock Loops – A Second Approach of the Fast Adaptive
Bandwidth Algorithm F. Legrand, C. Macabiau, ENAC, France, 408 The Impact of Proposed Pseudolite's Signal
Structure on the Receiver's Phase and Code Error I.F. Progri, W.R. Michalson, Worcester Polytechnic Institute, 414 Carrier Phase Processing Without Integers J.L. Farrell, VIGIL Inc., 423 Extended Kalman Filter Solution for Multiple
Hydrophone Position Calibration H.S. Wassaf, Lucent Technologies; H.J. Rome, U.
Mass Lowell, 429 A New Attitude Algorithm for the INS Using Ring
Laser Gyros Y. Teng, M. Guo, Q. Liu, H. Yang, Y. Zhang, Tsinghua University, P.R. China; J. Li, Bashan Instrument Factory, P.R. China, 444 Solutions of GPS Measurements by the Fixed-Point
Iteration Technique S. Lim, Inha University, Korea, 449 An Investigation of the Pseudolite's Signal
Structure for Indoor Applications I.F. Progri, J.M. Hill, W.R. Michalson, Worcester Polytechnic Institute, 453 SESSION B3: NAVIGATION RECEIVER TECHNOLOGY Real Time Verification of Bit-Cell Alignment for
C/A Code Only Receivers J. Hill, W.R. Michalson, Worcester Polytechnic Institute, 463 Multipath Characterization Using Digital Phased
Arrays A. Brown, N. Gerein, L. Savage, NAVSYS Corporation, 469 Measuring Interchannel Bias in GPS Receivers G. Johnson, T. Zaugg, Raytheon, 477 A Novel Approach to Enhancing the Sensitivity of
C/A Code GPS Receivers P.A. Dafesh, T. Fan, The Aerospace Corporation, 481 Open Architecture GPS Receiver A. Jovancevic, A. Brown, S. Ganguly, M. Kirchner, S.
Zigic, Center
for Remote Sensing, Inc.; L.
Scott, LS
Consulting Inc.; P. Ward, NAVWARD GPS Consulting, 489 Combating Digitizing Errors in GNSS-Receivers A.J.R.M. Coenen, Delft University of Technology, The Netherlands, 501 SESSION C3: SPACE-BASED & REGIONAL AUGMENTATION SYSTEMS Ionospheric Threat Model Methodology for WAAS J. Blanch, T. Walter, P. Enge, Stanford University, 508 Trade Study of Improvements to the WAAS
Ionospheric Integrity Function for GNSS Landing System (GLS) R. Lejeune, M.B. El-Arini, The MITRE Corporation/CAASD; E. Altshuler, Raytheon Company; T. Walter, Stanford
University, 514 A Prototype 3-Frequency SBAS Receiver and Test
Results D.M. Akos, K. Gromov, T. Walter, P. Enge, Stanford University, 522 High Speed LORAN-C Data Communications - June
2001 Update B. Peterson, K. Dykstra, Peterson Integrated Geopositioning, LLC; P. Swaszek, University of Rhode Island; J.M. Boyer, United
States Coast Guard, 530 SESSION A4: TESTING OF ADVANCED NAVIGATION SYSTEMS Demonstration of NATO Standard, STANAG 4572: A
Standardised Open System Architecture Interface to Enable Simulator Testing of
Integrated GPS/Inertial Navigation (IN) Equipment J. Stevenson, Royal Air Force, UK; S.L. Saks, Aerospace
Corp; N. Boasman, Defence Research Agency, UK; G. Ramsay, BAE SYSTEMS, 547 GPS Satellite Simulator Validation Testing for
the GPS JPO S. Green, GPS JPO/U.S. Navy; C. Stroing, U.S.
Navy, SPAWAR Systems Center; E.
Weston, U.S. Navy, Naval Air Warfare Center; B. Wheaton, GPS JPO, 556 Advanced GPS Hybrid Simulator Architecture A. Brown, N. Gerein, NAVSYS Corporation, 564 Validation of IEC 2400 GPS Simulator for High
Dynamic RTK Applications K.B. Anthony, S.A. Mirsky, USAF, 46th Test Wing/TSWS, 572 Testing an Integrated INS/GPS/GPWS K. Sheard, BAE SYSTEMS, UK; B.
Lenett, Honeywell
International, 579 GPS Signal Degradation Analysis Using a Simulator G. MacGougan, G. Lachapelle, M.E. Cannon, G. Jee, University of Calgary, Canada; M. Vinnins, Defence Research Establishment Ottawa, Canada, 586 Further Critical Perspectives on Certain Aspects
of GPS Development and Use T.H. Kerr III, TeK Associates, 592 SESSION B4: MILITARY NAVIGATION SYSTEMS Development of a Small Precision FOG IMU R. Valeri, E. Arnn, Raytheon; I.
Humphery, C. Reynolds, Fibersense
Technology Corporation, 609 Impact of Mechanical Vibrations on the
Performance of Integrated Navigation Systems and on Optimal IMU Specification J. Wendel, G.F. Trommer, University of Karlsruhe, Germany, 614 SUO/SAS Geolocation Land Navigation Using
Multiple Integrated Sensors E. Jacobson, T. Lee, C. Popeck, Rockwell Collins; M. Martorana, ITT; S.
Sokolowski, CECOM, 622 Development of a Tactile Accessory to Provide
Non-Visual Haptic Navigation: Initial Results J. Kelly, M. Bousselot, J. Meyer, S. Phelps, T. Larson, Rockwell Collins International, 634 Burn-Out, A Rational Requirement Formulation for
Military GPS User Equipment R.W. Mahoney, S.L. Saks, G.M.. Shaw, The Aerospace Corp.; K.A. Fromm, ARINC, Incorporated; R.M. Reinhart, Centurion Wireless Technologies, Incorporated, 642 SESSION C4: GROUND-BASED AUGMENTATION SYSTEMS NDGPS Network Enhancments in FY01 L.W. Allen, United States Coast Guard Navigation Center; D.B. Wolfe, C.L. Judy, E.J. Haukkala, R.W. James, United States Coast Guard Command and Control
Engineering Center, 652 Test Results and Modeling of Military GPS Landing
System Guidance Quality and Availability I. Gallimore, J. Hansen, Sierra Nevada Corporation, 661 Development of Local Area Augmentation System
Siting Criteria D. Lamb, FAA William J. Hughes Technical Center, 669 Integrity Design and Updated Test Results for the
Stanford LAAS Integrity Monitor Testbed G. Xie, S. Pullen, M. Luo, P.-L. Normark, D. Akos, J.
Lee, P. Enge, Stanford
University; B. Pervan, Illinois Institute of Technology, 681 LAAS Sigma-Mean Monitor Analysis and Failure-Test
Verification J. Lee, S. Pullen, G. Xie, P. Enge, Stanford University, 694 Preliminary Analysis of Requirements for CAT IIIB
LAAS C.A. Shively, Center for Advanced Aviation System Development, The MITRE
Corporation, 705 SESSION D4: COMPONENTS & MICROMECHANICAL SENSORS FOR INERTIAL NAVIGATION SYSTEMS & THEIR INTEGRATION GPS/INS - A Very Different Way F. van Graas, Ohio University; J.L.
Farrell, VIGIL,
Inc., 715 The Key to Unlocking the Emerging Market for
Civil (and DoD) Applications of Navigation Technology: Cost Scalable Interface
Standardization A. Tetewsky, A. Soltz, T. Bogner, E. O'Neil, The Charles Stark Draper Laboratory, Inc., 722 Femtosecond Optical Parametric Oscillator Gyro X. Meng, J.-C. Diels, University of New Mexico, 733 Adapting an Open-Loop MEMS Accelerometer for
Gun-Launched Navigation J. Cole, A. Cunningham, Silicon Designs, Inc.; J. Tauscher, Microvision, Inc., 737 Advanced Spinning-Vehicle Navigation - A New
Technique in Navigation of Munitions J.H. Doty, Rockwell Collins, Inc., 745 Active Solid State Short Pulse Laser Gyroscope T.T. Dang, A. Stintz, J.-C. Diels, The University of New Mexico; Y. Zhang, Tsinghua University, P.R. China, 755 Investigation on the High Frequency Readout
System for Dithering Ring Laser Gyros M. Guo, H. Yang,Y. Teng,Y. Zhang, Tsinghua University, P.R. China, 765 SESSION A5: SURVEYING, GEODETIC, MAPPING, & REMOTE-SENSING
APPLICATIONS USING GPS Availability Aspects of a Terrain Database
Integrity Monitor J. Campbell, M. Uijt de Haag, Ohio University; R. Gray, Penn
State University, 770 Space-Borne GPS Receivers for Remote Sensing of
the Ionosphere and the Troposphere S. Ganguly, A. Brown, A. Jovancevic, M. Kirchner, S.
Zigic, Center
for Remote Sensing, Inc., 778 Static Azimuth Determination Using a Single
Handheld GPS Receiver J. Kelly, E. Bogensberger, E. Rammelsberg, Rockwell Collins International, 790 SESSION B5: RANGE, REMOTE POSITIONING & TRACKING APPLICATIONS USING GPS GPS Network Implementation for Missile Defense
Testing A.W. Sutter, J.P. Cunningham, Naval Surface Warfare Center, Dahlgren Division,
797 A Space Based Internet Protocol System for Launch
Vehicle Tracking and Control B. Bull, D. Morgan, NASA, Goddard Space Flight Center; C. Grant, R. Streich, NASA, Computer Sciences Corporation, 809 Development of the GPS-Based Ballistic Missile
Range Safety Technology (BMRST) System C. Nesbit, D. Huff, Honeywell International; S. Croopnick, Draper Laboratories; R. Ostroff, ENSCO, Inc.; C.
Bartone, Avionics
Engineering Center, Ohio University; S. Slivinsky, Air Force Research Laboratory; C. Wilborn, Aero
Thermo Technology, Inc.; R.
Schoefield, Florida
Air National Guard, 816 A Portable Impact Location System D. Guilford, Palisades Geophysical Institute, Inc.; M.A. Cardoza, Applied Research Laboratories: The Univ. of Texas at Austin, 823 Aircraft Flight Evaluation of a Ballistic Missile
Range Safety Technology (BMRST) System C.G. Bartone, A. Wilson, Avionics Engineering Center, Ohio University, C. Nesbit, Honeywell International, R. Phillips, Draper Laboratory; R. Rexrode, ENSCO,
Inc., 829 SESSION C5: MILITARY PRECISION APPROACH & LANDING SYSTEMS Test Results of an F/A-18 Automatic Carrier
Landing Using Shipboard Relative GPS J. Waters, USN; P.
Sousa, L. Wellons, G. Colby, Naval Air Systems Command; J. Weir, J.F.
Taylor, Inc., 841 Guidance and Control for Shipboard Automatic
Landing Using GPS E.C. Schug, J.W. Aksteter, Scientific Applications International Corporation; R.W. Huff, Sierra Nevada Corporation; M.P. Smith, U.S.
Navy, 852 Use of Inertial Reference Data to Support
Differential GPS for Carrier Landing C.P. Bruner, Northrup Grumman Corporation, Litton Guidance & Control
Division; R.W. Breslau, Consultant to the Naval Air Weapons Center, 863 Test Results from a Digital P(Y) Code
Beamsteering Receiver for Multipath Minimization A. Brown, N. Gerein, NAVSYS Corporation, 872
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