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Open AccessJournal Article

Global Positioning System : Theory and Applications I

B. W. Parkinson
- 01 Jan 1996 - 
- Vol. 163, pp 3-55
TLDR
Differential GPS and Integrity Monitoring differential GPS Pseudolites Wide Area Differential GPS Wide Area Augmentation System Receiver Autonomous Integrity Monitoring Integrated Navigation Systems Integration of GPS and Loran-C GPS and Inertial Integration Receiver Aut autonomous Integrity Monitoring Availability for GPS Augmented with Barometric Altimeter Aiding and Clock Coasting
Abstract
Differential GPS and Integrity Monitoring Differential GPS Pseudolites Wide Area Differential GPS Wide Area Augmentation System Receiver Autonomous Integrity Monitoring Integrated Navigation Systems Integration of GPS and Loran-C GPS and Inertial Integration Receiver Autonomous Integrity Monitoring Availability for GPS Augmented with Barometric Altimeter Aiding and Clock Coasting GPS and Global Navigation Satellite System (GLONASS) GPS Navigation Applications Land Vehicle Navigation and Tracking Marine Applications Applications of the GPS to Air Traffic Control GPS Applications in General Aviation Aircraft Automatic Approach and Landing Using GPS Precision Landing of Aircraft Using Integrity Beacons Spacecraft Attitude Control Using GPS Carrier Phase Special Applications GPS for Precise Time and Time Interval Measurement Surveying with the Global Position System Attitude Determination Geodesy Orbit Determination Test Range Instrumentation.

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Citations
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Dissertation

Investigation of MEMS inertial sensors and aircraft dynamic models in global positioning system integrity monitoring for approaches with vertical guidance

TL;DR: This research investigates fusing GPS with lower-cost Micro-Electro-Mechanical System (MEMS) Inertial Measurement Units (IMU) and a mathematical model of aircraft dynamics, referred to as an Aircraft Dynamic Model (ADM) in this thesis, to investigate its use in Aircraft Based Augmentation Systems (ABAS).
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Reference satellite selection method for GNSS high-precision relative positioning

TL;DR: This work introduces condition number of the design matrix in the reference satellite selection method to improve structure of the normal equation and shows that the new method can improve positioning accuracy and reliability in precise relative positioning.

Sequential RAIM designed to detect combined step ramp pseudo-range errors

TL;DR: The results obtained show that the robustness of the existing techniques has been improved by the proposed snapshot and sequential RAIM FDE algorithms based on the constrained Generalized Likelihood Ratio (GLR) test.
Journal Article

Error Reduction for GPS Accurate Timing in Power Systems using Kalman Filters and Neural Networks

TL;DR: The experimental results obtained from a Coarse Acquisition (C/A)-code single-frequency GPS receiver strongly support the potential of the method using PSNN to give high accurate timing, and the GPS timing RMS error reduces to less than 38 nanoseconds.
Journal ArticleDOI

Asynchronous Pseudolite Navigation Using C/N0 Measurements

TL;DR: It is demonstrated that metre level accuracy can be achieved using asynchronous pseudolites, and these results are particularly encouraging since they were obtained without exploiting map constraints and prior knowledge of the user position.
References
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Wide Area Differential GPS

TL;DR: Simulation results indicate that normal GPS positioning errors can potentially be reduced by more than 95% using WADGPS.

Ephemeris and Clock Navigation Message Accuracy

J. Zumberge, +1 more
TL;DR: The accuracy of the ephemeris and clock corrections contained in the GPS navigation message is discussed.

GPS and Inertial Integration

TL;DR: This chapter devotes one section to address each of the following questions: how complex are the integration algorithms required to provide the desired level of performance, with options for growth to meet future requirements?

Test Range Instrumentation

TL;DR: In the early 1970s, laser trackers became available to support test activities as discussed by the authors, and a combination of radar, distance-measuring equipment (DME), optical trackers such as cinetheodolites, and other miscellaneous instrumentation to provide time-space position information (TSPI) to satisfy test platform positioning requirements.