1996 National Technical Meeting Proceedings Plenary Session Operational Status of Navigation Technologies Operational Status of Loran Dale Johnson, International Loran Association 3-5 Operational Status of Inertial Neil Barbour, C. S. Draper Laboratory 7-15 Operational Status of GNSS Keith McDonald, Sat Tech Systems 17-23 Session A1: Aviation: GPS Based Landing Guidance GPS Receiver Tracking Loop Modeling to Support Autoland Simulations M. Braasch, Ohio University; G. McGraw, Rockwell-Collins 27-33 DGPS Multlchannel Autoland System Performance U. Wacker, Daimler-Benz Aerospace; A. Both, Rockwell-Collins 35-43 Development of the Unified Risk Model for Evaluation of Current and Future Airspace H. J. Rome, University of Massachusetts 45-59 Session A2: Integrated Navigation High Performance GGP for Multiple Dual-Use Applications N. Dahien, T. Caylor, E. Goldner, Litton 0 & C Systems 63-74 MIT Kit for Multifunctional Target Instrumentation C. Yang, Signal and System Technologies 75-82 A Super-Fast Integer Ambiguity Resolution Approach to GPS Interferometric Heading Determination for the Application in a Low Cost Integrated GPS/Inertial System R. K. Li, Lear Astronics Corporation 83-88 Session A3: Military Applications Benign GPS Selective Availability (SA) Paradigms for Dual-Use GPS D. Latterman, US Air Force; B. Mathers, US Navy; J. Malapit, US Army 91-105 GPS ISU D. Hiorth, ERI 107-114 Simulating the GPS Constellation for High Fidelity Operator Training R. Hazelhurst, D. Greenhut, R. Walker, Loral Federal Systems; L. Come, USAF 115- 123 Session B1: Aviation: GPS Based Landing Guidance DGPS Category IIIb Feasibility Demonstration - Landing System with Flight Test Results G. Romrell, R. Brown, G. Johnson, E-Systems; D. Kaufmann, NASA Ames 127-136 GPS Multipath on Large Commercial Air Transport Airframes T. Murphy, R. Snow, Boeing; M. Braasch, Ohio University 137-143 Test Results of Local Area Augmentation of GPS with an In-band Pseudolite B. Elrod, K. Barltrop, J. Stafford, D. Brown, Stanford Telecommunications 145-154 The Boeing/Industry GPS Landing System Flight Test Experiments Session C2: Marine Bringing a Full Mission Bridge Simulator on Line-The Human Factor J. Buckley, P. Leyda, California Maritime Academy 369-376 Expected Safety Benefits of Electronic Charts and Integrated Navigation Systems H. Kite-Powell, D. Jin, S. Farrow, Woods Hole Oceanographic Institution 377-385 Global Navigation Satellite System Requirements for Vessel Traffic Services W.R. Cairns, J.M. Sollosi, US Coast Guard 387-398 Evaluation of High Performance Multipath Reduction Technologies for Precise DGPS Shipborne Positioning G. Lachapelle, A. Bruton, J. Henriksen, M.E. Cannon, The University of Calgary 399-406 Implementation and Assessment of a Low Cost Shipboard Bridge Team Training Simulator Using Virtual Reality Technology R. Quinn, US Coast Guard Academy; S. Conway, US Coast Guard 407-411 Navigation Automation—Completing the Cycle J. Beukers, Beukers Technology; W. Roland, Megapulse, Inc 413-420 Session C3: International and GNSS Performance Comparisons Between GPS and GLONASS Transmission Systems A. Benhallam, R. Rosso, Ecole Nationale de l’Aviation Civile 423-430 Development of the European Radio Navigation Plan (ERNP) L. Tytgat, European Commission; A. Nelson, Booz Allen & Hamilton; W. Lechner, Avionik Zentrum; W. Blanchard, FRIN 431-435 Report on the International Workshop on GPS Interference B. Davies, European Systems; R. Johannessen, Lambourne Navigation; M. Saville, Northern Lighthouse Board 437-441 Designing a Multimodal GNSS Based on Optimal Cost Efficiency to All Users J. Doble, Booz Allen & Hamilton 443-445 GLONASS Integrity Monitoring by Internet N. Zarraoa, W. Mai, H. Daedelow, A. Jungstand, DLR-DFD 447-451 CNS/ATM In China: Developing a Path to the Future J. Estill, Q. Zhihe, Rockwell 453-460 Session D1: Space: Orbit/Rendezvous Applications Single Frequency GPS Orbit Determination for Low Earth Orbiters S-C. Wu, W. Bertiger, Jet Propulsion Laboratory 463-473 Real Time Data Acquisition of Missile Position Using Spacecraft Passive (Infrared) Sensor and GPS Integrated Angular Rate Positioning System A. Murakami, GPS Hand-Set Design Shop 475-491 Integration of Low Earth Orbit Satellite Data Communications Services with Maritime Navigation and Positioning Systems R. Kelly, ORBCOMM 493-499 Spacecraft Rendezvous by GPS-Derived Range and Attitude H. Satz, Independent Consultant 501-508 MicroGPS for Orbit Determination of Earth Satellites S-C. Wu, W. Bertiger, A. Reichert, J. Srinivasan, JPL 509-516 Autonomous Deterministic Spacecraft Positions Using the Magnetic Field and Attitude Information E. Ketchum, NASA Goddard Space Flight Center 517-526 Session D2: Aviation: Airport Landing and Surface Guidance APALS(tm) Program Status and Pre-Production Unit flight Test Results O. Dieffenbach, Lockheed Martin 529-535 Augmenting Kinematic GPS With a Pulsed Pseudolite to Improve Navigation Performance D. Lawrence, B. Pervan, S. Cobb, C. Cohen, J.D. Powell, B. Parkinson, Stanford University 537-545 New Innovative Low-Cost Precision Landing System J. Stoltz, D. Frazier, Advanced Navigation & Positioning Corporation; L.N. Spohnheimer, FAA 547-554 Improved Location/Identification of Aircraft/Ground Vehicles on Airport Movement Areas-Results of FAA Trials R. Castaldo, FAA; C. Evers, Rannoch Corp 555-562 A Demonstrated Solution for Satisfying ICAO’s All Weather Operations Panel (AWOP) Airport Operational Requirements Using Seamless Airport Independent GNSS Processing Techniques B. Pulley, DSDC 563-578 Planning and GNSS-based Monitoring of On-Ground Aircraft Movements F. Weiczer, Chalmers University of Technology; L. Johnsson, Swedish/CAA 579-584 Session E1: Surveying and Precise Positioning Robust Differential GPS Processing Using Jupiter(tm): Algorithms and Results Y. Gao, J.F. McLellan, M. Forkheim, Pulsearch Navigation Systems 587-595 Integer Ambiguity Search: What Is the Point? R.K Li, Lear Astronics 597-604 Development of a Real-Time Kinematic System: System Design, Performance and Result H. Lan, M.E. Cannon, The University of Calgary 605-613 An Assessment of Predicted and Measured Ionospheric Total Electron Content Using a Global GPS Network A. Komjathy, R. Langley, University of New Brunswick 615-624 GPS Ionosphere Determination Using Li Only P Nisner, UK CAA NATS; M. Trethewey, Signal Computing Ltd 625-635 Session E2: Aviation Landing Guidance WAAS Avionics Receiver Design Characteristics R. Kumar, P. Munjal, K.T. Woo, H. Yeh, The Aerospace Corp 639-654 GPS Signal Environment, Passive Monitoring System P. Manning, TASC; P. McCarty, J. Ruggiero, Unisys; W. Mason, B. Winer, Volpe Center; R. Frazier, FAA 655-658 Long Range Differential Corrections Transmission for Airborne GNSS-based Guidance Systems M. Dieroff, G. Sachs, D. Dittrich, Technische Universität 659-667 GPS Receiver RFI Laboratory Tests M. Geyer, A. Cameron, P. Manning, TASC; P McCarty, J. Ruggiero, Unisys; W. Mason, B. Winer, Volpe Center; R. Frazier, FAA 669-676 Test Results of the Joint FAA/DOD Investigation of the GPS Interference M. Shaw, FAA; K. Sandhoo, The MITRE Corp.; R. Cole, Innovative Solutions International; G. Colby, Naval Air Warfare Center 677-686 Session E3: Space: Special Techniques Past & Future Passive Ranging Navigation R. Easton and R. Anderson 689-698 REQUEST-A New Recursive Algorithm for Attitude Determination I.Y. Bar-Itzhack, NASA GSFC 699-706 Method for Calculating Multipath Environment and Impact on GPS Receiver Solution Accuracy W. Lippincou, Naval Research Lab; T. Milligan, D. Igli, Lockheed Martin Astronautics 707-722 Effects of Antenna Pattern on GPS Phase Measurement in Space Station Environment |
