1999 National Technical Meeting Proceedings Table Of Contents Plenary Session KEYNOTE ADDRESS, J. Hull, Director of Operations Policy Directorate, U.S. Coast Guard, page 3. GLOBAL POSITIONING SYSTEM: A POLICY PERSPECTIVE, S. Moran, Office of Science & Technology Policy, Executive Office of the President, page 7. NAVSTAR GLOBAL POSITIONING SYSTEM, J. Armor, GPS JPO, page 13. GPS FUTURE OPTIONS, A PERSPECTIVE, L.K. Lewis, Institute for Defense Analysis, page 21. GPS: THE NEXT STEP!, K. Chadha, SiRF Technology, page 39. Session A1-National/International Systems & Issues OVERVIEW OF SYSTEM ARCHITECTURAL IMPLICATIONS OF THIRD PARTY LIABILITY AND GOVERNMENT INDEMNIFICATION FOR GLOBAL POSITIONING SYSTEM AUGMENTATION, J. R. Copeland, The Aerospace Corporation, page 65. FLIGHT INSPECTION OF GPS PROCEDURES PAST, PRESENT, AND FUTURE, G. C. Keedy, Flight Inspection Policy and Standards, FAA, page 75. GPS DEFINITIONS, A. Pinker, ANSER, page 83. GPS SUPPLEMENTAL NAVIGATION SYSTEMS FOR USE DURING THE TRANSITIONTO A SOLE-MEANS-GPS NATIONAL AIRSPACE SYSTEM, D. Gebre-Egziabher, S. Lo, J. D. Powell, P. Enge, Stanford University, page 91. GPS GROUND CONTROL NETWORK MODERNIZATION, R. Harker, Z. Nelson, Lockheed Martin Mission Systems, page 101. ON NEW SIGNAL STRUCTURES FOR GNSS-2, R. Schweikert, T. Woerz, Audens ACT Consulting GmbH,Germany, R. De Gaudenzi,European Space Agency, page 109. IONOSPHERIC DELAY USING ONLY LI: VALIDATION AND APPLICATION TO GPS RECEIVER CALIBRATION AND TO INTER-FREQUENCY BIASES ESTIMATION, R. Moreno, N. Suard, Centre National d'Estudes Spatiales-CNES, page 119. Session A2-Aviation Applications LAAS MONITORING FOR A MOST EVIL SATELLITE FAILURE, A. Mitelman, J. Jung, P. Enge, Stanford University, page 129. AIRPORT MULTIPATH SIMULATION FOR SITING DGPS REFERENCE STATIONS, C. Macabiau, B. Roturier, CNS Research Laboratory of the ENAC; E. Chatre, STNA; A. Renard, Sextant Avionique, page 135. THE DEVELOPMENT AND TESTING OF A WAAS VERIFICATION RECEIVER, T. Sanders, ARINC; R. Brinkley, T. Lardy, NAWC-AD, page 145. TWO ANTENNA GPS ATTITUDE AND INTEGER AMBIGUITY RESOLUTION FOR AIRCRAFT APPLICATIONS, R. Hayward, A. Marchick, J. D. Powell, Aero/Astro Dept., Stanford University, page 155. BOUNDING MULTIPATH ERRORS INDUCED BY ELECTRONIC COMPONENTS IN RECEIVER HARDWARE, J. Keith, 746th Test Squadron, Holloman AFB, NM, page 165. LONG BASE REAL TIME POSITIONING OF AIRBORNE SENSORS, P. Tome, T. Cunha, S. Cunha, L. Bastos, Astronomical Observatory of the University of Porto, Portugal, page 173. Session A3-Charting, Mapping, & Surveying ACHIEVABLE GPS MULTIPATH MITIGATION PERFORMANCE USING DUAL CIVIL FREQUENCIES, L. Weill, California State University, Fullerton, page 181. REAL-TIME GPS REFERENCE NETWORK CARRIER PHASE AMBIGUITY RESOLUTION, H. Sun, T.E. Melgard, Kvaerner Marine Automation; M.E. Cannon, The University of Calgary, page 193. GEOMETRY-FREE AMBIGUITY SUCCESS RATES IN CASE OF PARTIAL FIXING, P.J.G. Teunissen, P. Joosten, C.C.J.M. Tiberius, Delft University of Technology, page 201. KINEMATIC MAPPING WITH GPS IN THE DESERT, A. El-Mowafy, United Arab Emirates University, page 209. THE GPS DATA WEIGHT MATRIX: WHAT ARE THE ISSUES?, C.C.J.M. Tiberius, Delft University of Technology, page 219. Session A4-Strategic and Tactical Weapons Test & Evaluation ANALYSIS OF WADGPS POSTFLIGHT NAVIGATION SOLUTIONS FOR VANDAL AND HERA MISSILE TESTS, J. Cunningham, A. Evans, B. Hermann, NSWCDD; B. Remondi The XYZ's of GPS, Inc; J. Merts, Eglin Air Force Base, page 231. DESIGN AND PERFORMANCE OF A C/A CODE RECEIVER FOR PROJECTILE REGISTRATION, J. Price, Army Research Laboratory AMSRL-SE-SA, page 241. MULTIFUNCTIONAL INSTRUMENTATION FOR TARGETS: PRELIMINARY GROUND TEST RESULTS, C. Yang, Signal & System Technologies, page 251. DOD METHODOLOGY, PAST VS. FUTURE, J. Farrell, VIGIL Inc., page 259. Session B1-Expansion/Augmentation Issues GPS CONSTELLATION STATE PROBABILITIES, HISTORICAL AND PROJECTED, C. Kelley, Boeing, page 265. NON-PRECISION APPROACH AVAILABILITY SENSITIVITY TO GPS SATELLITE CONSTELLATION CONFIGURATION, J.-S. Wu, N. Pandya, J. Lewellen, Raytheon System Company; J. Angus, Claremont Graduate University, page 271. WAAS MOPS: PRACTICAL EXAMPLES, T. Walter, Stanford University, page 283. ANALYSIS OF CODE CROSS CORRELATION NOISE IN GPS RECEIVERS OPERATING IN AUGMENTED GPS SYSTEMS, R. Kumar, S. Raghavan, M. Zeitzew, P. Munjal, S. Lazar, The Aerospace Corporation, page 295. ANALYSIS OF PROBABILITY OF MISLEADING INFORMATION FOR LAAS SIGNAL IN SPACE, C. Shively, The MITRE Corporation, page 305. NEW CONCEPTS FOR A CARRIER PHASE BASED GPS POSITIONING USING A NATIONAL REFERENCE STATION NETWORK, B. Townsend, Consultant (KMA); G. Lachapelle, L. Fortes, The University of Calgary; T.E. Melgard, Kvaerner Marine Automation; T. Norbech, Norwegian Mapping Authority; J. Raquet, AFIT, Wright-Patterson AFB, page 319. Session B2: GPS Interference Issues and Testing CLASSIFIED SESSION. For more information on obtaining classified proceedings of this session please contact: Mr. Philip B. Simpson, 746th Test Squadron/TGGPA, 1644 Vandergrift Road, Holloman AFB, NM 88330-7850; Phone: 505-679-1756 (DSN 349); Fax: 505-679-1645 (DSN 349); Email: psimpson@mailgate.46tg.af.mil. Session C1-Land Applications NEXT-GENERATION OF HANDHELD GPS PRODUCTS WILL REQUIRE NEXT GENERATION DISPLAYS, G. Kephart, Kopin Corporation, page 329. GNSS MULTIPATH MITIGATION USING GATED AND HIGH RESOLUTION CORRELATOR CONCEPTS, G. McGraw, Rockwell Collins; M. Braasch, Ohio University, page 333. CHARACTERIZATION OF GPS CARRIER PHASE MULTIPATH, J.K. Ray, M.E. Cannon, University of Calgary, page 343. INTEGRATED DR/DGPS USING LOW COST GYRO AND SPEED SENSOR, R. Rogers, Rogers Engineering & Associates, page 353. AN INTEGRATED VEHICLE POSITIONING SYSTEM FOR SAFETY APPLICATIONS, S. Weisenburger, C. Wilson, DaimlerChrysler Research and Technology Center, Palo Alto, page 361. DEVELOPMENT OF A LOW COST SYSTEM FOR THE AUTOMATED DOCUMENTATION OF CRASH SCENES USING GPS (AUTODOCS-GPS), C. Rodgers, D. Greenlee, OPTIMUS Corporation, page 369. Session C2-Navigation Warfare (NAVWAR) CLASSIFIED SESSION. For more information on obtaining classified proceedings of this session please contact: Mr. Philip B. Simpson, 746th Test Squadron/TGGPA, 1644 Vandergrift Road, Holloman AFB, NM 88330-7850; Phone: 505-679-1756 (DSN 349); Fax: 505-679-1645 (DSN 349); Email: psimpson@mailgate.46tg.af.mil. Session D1-Integration of Navigation Systems INTEGRATING MULTIPLE GPS RECEIVERS WITH A LOW COST IMU FOR AIRCRAFT ATTITUDE DETERMINATION, P. Tome, T. Cunha, S. Cunha, L. Bastos, Astronomical Observatory of the University of Porto, Portugal, page 379. DEVELOPMENT AND TESTING OF A RELATIVE GPS BASED SYSTEM FOR GUIDANCE IN PRECISION APPROACH & LANDING ON AIRCRAFT CARRIERS, M. Toledo, J.C. Bastante, GMV S.A., page 387. THE DETERMINATION OF GRAVITY DATA SPACING REQUIRED FOR INERTIAL NAVIGATION, R. Anderson, J. Davenport, National Imagery and Mapping Agency; C. Jekeli, Ohio State University, page 399. FLIGHT TRIALS OF A GEOSTATIONARY SATELLITE BASED AUGMENTATION SYSTEM AT HIGH LATITUDES AND FOR DUAL SATELLITE COVERAGE, R. Fuller, Todd Walter, S. Houck, P. Enge, Stanford University, page 405. GPS PSEUDOLITE TRANSCEIVERS AND THEIR APPLICATIONS, J. Stone, E. LeMaster, J.D. Powell, S. Rock, Stanford University, page 415. NEW LORAN CAPABILITIES ENHANCE PERFORMANCE OF HYBRIDIZED GPS/LORAN RECEIVERS, G.L. Roth, P. Schick, Locus, Inc., page 425. A PHYSICAL THEORY OF DIFFRACTION MODEL FOR PREDICTING THE EFFECTS OF MULTIPATH ON ILS AND VOR PERFORMANCE, S. Odunaiya, Ohio University, page 435. OPTIMAL USE OF BOTH GPS CARRIER AND CODE TRACKING OBSERVATIONS, J. Lukesh, Retired from Northrop Grumman, page 447. INTEGRATION OF A REAL-TIME GPS DATA COLLECTION NETWORK WITH A VARIETY OF CUSTOMER APPLICATIONS, B. Renfro, R. Mach, J. Little, The University of Texas at Austin; T. Creel, R. Taylor, NIMA, page 455. Session D2-Marine Applications GPS-BASED VESSEL TRAFFIC MANAGEMENT AT THE PANAMA CANAL, W. Keepers, Panama Canal Commission; J. Carroll, U.S. DOT/Volpe National Transportation Systems Center, page 465. DEMONSTRATION PROJECT RESULTS OF GPS C WIDE-AREA GPS CORRECTIONS FOR REMOTE AREAS INCLUDING THE ARCTIC, K. Lochhead, M. Caissy, K. MacLeod, F. Lahaye, P. Heroux, Geodetic Survey Division, Geomatics Canada; R. Doucett, Canadian Coast Guard, page 471. ELECTRONIC NAVIGATION ON THE COAST GUARD'S MEDIUM ENDURANCE CUTTERS, D. Ronan, T. Routhier, USCG; J. Ryan, USMM, page 477. DETERMINATION OF INTEGRATED NAVIGATION SYSTEM REQUIREMENTS FOR A SHALLOW WATER AUV USING OFF THE SHELF HARDWARE, P. Franco, M. Levrant, E. Nosenchuk, Applied Research Lab, The Pennsylvania State University, page 489. RTK-GPS POSITIONING IN JAPAN BY GPS-BASED CONTROL STATIONS VIA DMCA RADIO COMMUNICATION SYSTEM, H. Namie, N. Tanaka, A. Yasuda, Tokyo University of Mercantile Marine, page 495. TESTING AND ANALYSIS OF RELIABILITY MEASURES FOR GNSS RECEIVERS IN THE MARINE ENVIRONMENT, S. Ryan, J. Stephen, G. Lachapelle, University of Calgary, page 505. A METHODOLOGY FOR MODELING THE PSEUDORANGE MEASUREMENTS, L.C.L. Rosa, F. Walter, L.H.P.M. Alves, ITA, page 515. Session D3-Space Technology MULTIPATH ERROR ANALYSIS AND CALIBRATION FOR GPS DIFFERENTIAL PHASE, J. Godet, J. Dantepal, M. Grondin, D. Belot, L. Baudenon, C. Sourdois, I. Sebbag, C.N.E.S., page 521. USAGE OF TWO-DIRECTIONAL LINK TECHNIQUES FOR DETERMINATION OF THE SATELLITE STATE FOR GNSS-2, J. Hammesfahr, A. Hornbostel, J. Hahn, H. Trautenberg, C. Rapp, W. Specht, DLR e.V., Germany; B. Eissfeller, R. Wolf, O. Balbach, T. Zink, Z. Fu, IfEN, Germany; H. Malthan, N. Lemke, Kayser-Threde GmbH, Germany; P. Souty, D. Levavasseur,Dassault Electronique, France; W. Schafer, TimeTech GmbH, Germany; P. Tavella, M. Leonardi, IEN, Italy, page 531. GPS RECEIVER SATELLITE/ANTENNA SELECTION ALGORITHM FOR THE STANFORD GRAVITY PROBE B RELATIVITY MISSION, J. Li, A. Ndili, S. Buchman, Stanford University; L. Ward, Ball Aerospace & Technologies Corporation, page 541. AN INNOVATIVE GPS SOLUTION FOR THE ORBCOMM CONSTELLATION SPACECRAFT, B. Patel, Orbital Sciences Corporation; W. Walter, ORBCOMM Global LP; D. Patton, EON Corporation, page 551. REDUCING THE POWER REQUIREMENTS OF AN INTERFEROMETRIC GPS RECEIVER FOR SPACECRAFT ATTITUDE DETERMINATION, W. Guinon, R. Setterlund, R. Phillips, Draper Laboratory, page 561. GPS SIGNALS IN A GEOSYNCHRONOUS TRANSFER ORBIT: "FALCON GOLD" DATA PROCESSING, T. Powell, P. Martzen, S. Sedlacek, C.-C. Chao, The Aerospace Corporation; R. Silva, A. Brown, NAVSYS Corporation; G. Belle, USAF Academy, page 575. GPS-BASED POSITION DETERMINATION FOR GEOSYNCHRONOUS SATELLITES, R. Bryan, Scitor Corporation, page 587. Session D4-GPS User Equipment Test and Evaluation MULTIPATH ERROR ANALYSIS AND CALIBRATION FOR GPS DIFFERENTIAL PHASE, J. Godet, J. Dantepal, M. Grondin, D. Belot, L. Baudenon, C. Sourdois, I. Sebbag, C.N.E.S., page 521. USAGE OF TWO-DIRECTIONAL LINK TECHNIQUES FOR DETERMINATION OF THE SATELLITE STATE FOR GNSS-2, J. Hammesfahr, A. Hornbostel, J. Hahn, H. Trautenberg, C. Rapp, W. Specht, DLR e.V., Germany; B. Eissfeller, R. Wolf, O. Balbach, T. Zink, Z. Fu, IfEN, Germany; H. Malthan, N. Lemke, Kayser-Threde GmbH, Germany; P. Souty, D. Levavasseur,Dassault Electronique, France; W. Schafer, TimeTech GmbH, Germany; P. Tavella, M. Leonardi, IEN, Italy, page 531. GPS RECEIVER SATELLITE/ANTENNA SELECTION ALGORITHM FOR THE STANFORD GRAVITY PROBE B RELATIVITY MISSION, J. Li, A. Ndili, S. Buchman, Stanford University; L. Ward, Ball Aerospace & Technologies Corporation, page 541. AN INNOVATIVE GPS SOLUTION FOR THE ORBCOMM CONSTELLATION SPACECRAFT, B. Patel, Orbital Sciences Corporation; W. Walter, ORBCOMM Global LP; D. Patton, EON Corporation, page 551. REDUCING THE POWER REQUIREMENTS OF AN INTERFEROMETRIC GPS RECEIVER FOR SPACECRAFT ATTITUDE DETERMINATION, W. Guinon, R. Setterlund, R. Phillips, Draper Laboratory, page 561. GPS SIGNALS IN A GEOSYNCHRONOUS TRANSFER ORBIT: "FALCON GOLD" DATA PROCESSING, T. Powell, P. Martzen, S. Sedlacek, C.-C. Chao, The Aerospace Corporation; R. Silva, A. Brown, NAVSYS Corporation; G. Belle, USAF Academy, page 575. GPS-BASED POSITION DETERMINATION FOR GEOSYNCHRONOUS SATELLITES, R. Bryan, Scitor Corporation, page 587. Session E1-Future of GPS THE OFFSET CARRIER MODULATION FOR GPS MODERNIZATION, J. Betz, The MITRE Corporation, page 639. COHERENT ADAPTIVE SUBCARRIER MODULATION (CASM) FOR GPS MODERNIZATION, P. A. Dafesh, T. M. Nguyen, S. Lazar, The Aerospace Corporation, page 649. ANALYSIS OF PROPOSED GPS SIGNAL STRUCTURES FOR USE IN ARNS BANDS, A.J. Van Dierendonck, AJ Systems; P. Reddan, Zeta Associates, Inc., page 661. TRACKING ALGORITHM FOR GPS OFFSET CARRIER SIGNALS, P. Fine, W. Wilson, The MITRE Corporation, page 671. A STUDY OF LINEAR PHASE COMBINATIONS IN CONSIDERING FUTURE CIVIL GPS FREQUENCIES, S. Ericson, The MITRE Corporation, page 677. SPECIFICATIONS TO OBTAIN CATEGORY I PRECISION APPROACH WORLDWIDE, C. Kelley, Boeing, page 687. MANAGEMENT OF GPS, A. Pinker, S. Adams, C. Beirne, ANSER, page 695. Session E2-Integrated Systems SEPARATING VERTICAL DEFLECTION FROM ATTITUDE ERRORS BY PROPER GRAVITY MODELING IN A TIGHTLY INTEGRATED GPS/INS SYSTEM, J. Wang, The Ohio State University Center for Mapping, page 709. GYROCOMPASS ALIGNMENT WITH BASE MOTIONS - RESULTS FOR A 1-NMI/HR INS/GPS SYSTEM, C. Hua, Trimble Aerospace, page 717. ATTITUDE DETERMINATION USING GPS CARRIER PHASE AND COMPASS DATA, H. M. Peng, F. R. Chang, Dept. of Elec. Eng., National Taiwan University; L. S. Wang, Inst. of Applied Mechanics, National Taiwan University, page 727. OPEN SYSTEM STANDARDS FOR TIGHTLY INTEGRATED GPS/PCS SYSTEMS: ISSUES AND TRADES, R. DiEsposti, S. Saks, The Aerospace Corporation, page 733. FLIGHT TEST RESULTS IN A PROGRAM TO DEVELOP NEW TERMINAL INSTRUMENT PROCEDURES TERPS FOR PRECISION AND WAAS APPROACHES, H. Hejjo, J. Fagan, E. Darne, University of Oklahoma; R. Sexton, Innovative Solutions International; G. McCartor, FAA, page 741. A LOW COST ADAPTIVE ANTENNA ARRAY, J.Blas, R. Blazquez, J. Alonso, Universidad Politecnica de Madrid, page 751. Session E3-Atmospheric Effects DETERMINING THE UNCERTAINTY OF IONOSPHERIC CORRECTIONS FOR USERS IN WIDE AREA AUGMENTATION SYSTEMS, A.J. Mannucci, C.M. Ho, B.A. Iijima, U. Lindqwister, X. Pi, B.D. Wilson, Jet Propulsion Laboratory, California Institute of Technology, page 761. THE EFFECTS OF LOCAL IONOSPHERIC DECORRELATION ON LAAS: THEORY AND EXPERIMENTAL RESULTS, J. Christie, A. Hansen, D. Dai, S. Pullen, B. Parkinson, Stanford University; P.Y. Ko, Chung Shan Institute of Technology and Science; B. Pervan, Chicago Institute of Technology, page 769. NATIONAL SATELLITE TEST BED (NSTB) OBSERVATIONS OF THE EFFECTS OF IONOSPHERIC STORMS ON A PROTOTYPE WIDE AREA AUGMENTATION SYSTEM, T. Dehel, K. Pham, J. Sheftic, FAA Technical Center; D. Nelthropp, Systems Resources Corporation, page 779. HIGH LATITUDE OBSERVATIONS OF IONOSPHERIC SCINTILLATION EVENTS USING THE NSTB, J. Nichols, A. Hansen, T. Walter, P. Enge, Stanford University, page 789. SCINTILLATION MODELING FOR GPS/WAAS RECEIVER, C. Hegarty, M. Bakry El-Arini, T. Kim, S. Ericson, The MITRE Corporation, page 799. IMPACT OF IONOSPHERIC SCINTILLATION ON GPS/WAAS SYSTEM AND ITS MITIGATION TECHNIQUES, R. Kumar, The Aerospace Corporation, page 809. Session E4-Timing and Current Receiver Initiatives DEFINITION AND ANALYSIS OF WAAS RECEIVER MULTIPATH ERROR ENVELOPES D. Cox, K. Shallberg, Zeta Associates Inc.; A. Manz, Novatel Communications Ltd, page 827. WAAS NETWORK TIME PERFORMANCE WITH SITE DATA, C. Griffith, S. Peck, Raytheon Systems Company; W. Bertiger, Jet Propulsion Laboratory, page 839. COMPREHENSIVE GPS RECEIVER EPOCH (Y2K, EOW) TESTING, C. Falchetti, C. Stroing, Spawar Systems Center; P. Bouniol, J.-P. Saulay, LRBA, page 847. GEO UPLINK SUBSYSTEM (GUS) CLOCK STEERING ALGORITHMS PERFORMANCE AND VALIDATION RESULTS, M. S. Grewal, California State University, Fullerton; W. Brown, R. Lucy, P.Hsu, Raytheon Systems Company, page 853. EFFECT OF ICE LOADING ON A GPS ANTENNA, K. O'Keefe, J. Stephen, G. Lachapelle, University of Calgary; R. Gonzales, Raytheon Systems, Fullerton, CA, page 861. STEERING THE U.S. NAVAL OBSERVATORY (USNO) MASTER CLOCK, D. Matsakis, M. Miranian, USNO; P. Koppang, Frequency and Time Systems, page 871. C/A CODE TRACKING AND ACQUISITION WITH INTERFERENCE REJECTION USING THE EXTENDED KALMAN FILTER, R. Iltis, University of California, Santa Barbara; G. Hanson, Naval Air Warfare Center, page 881. GPS RECEIVER TEST PLAN FOR WEEK ROLL OVER AND Y2K CRITICAL DATES COMPLIANCE, M.G. Petovello, G. Fotopoulos, M.E. Cannon, G. Lachapelle, The University of Calgary; S. Ryan, Canadian Coast Guard, page 891. |
