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dc.contributor.advisorSubbarao, Kamesh
dc.creatorCopp, Brian Lee
dc.date.accessioned2016-01-26T22:45:12Z
dc.date.available2016-01-26T22:45:12Z
dc.date.created2015-12
dc.date.issued2015-11-24
dc.date.submittedDecember 2015
dc.identifier.urihttp://hdl.handle.net/10106/25435
dc.description.abstractIt is well known that satellite navigation systems are vulnerable to disruption due to jamming, spoofing, or obstruction of the signal. The desire for robust navigation of aircraft in GPS-denied environments has motivated the development of feature-aided navigation systems, in which measurements of \textit{environmental features} are used to complement the dead reckoning solution produced by an inertial navigation system. Examples of environmental features which can be exploited for navigation include star positions, terrain elevation, terrestrial wireless signals, and features extracted from photographic data. Feature-aided navigation represents a particularly challenging estimation problem because the measurements are often strongly nonlinear, and the quality of the navigation solution is limited by the knowledge of nuisance parameters which may be difficult to model accurately. As a result, integration approaches based on the Kalman filter and its variants may fail to give adequate performance. This project develops a framework for the integration of feature-aided navigation techniques using Bayesian statistics. In this approach, the probability density function for aircraft horizontal position (latitude and longitude) is approximated by a two-dimensional point mass function defined on a rectangular grid. Nuisance parameters are estimated using a hypothesis based approach (Multiple Model Adaptive Estimation) which continuously maintains an accurate probability density even in the presence of strong nonlinearities. The effectiveness of the proposed approach is illustrated by the simulated use of terrain referenced navigation and wireless time-of-arrival positioning to estimate a reference aircraft trajectory. Monte Carlo simulations have shown that accurate position estimates can be obtained in terrain referenced navigation even with a strongly nonlinear altitude bias. The integration of terrain referenced and wireless time-of-arrival measurements is described along with preliminary results. In addition, a new Bayesian algorithm for visual navigation by feature tracking is presented. Finally, a unified framework for integration of feature-aided positioning techniques using Bayesian statistics is described.
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.subjectGPS denied navigation
dc.subjectTerrain referenced navigation
dc.subjectTime of arrival positioning
dc.subjectBayesian estimation
dc.subjectBayesian statistics
dc.titleBayesian Statistics and Information Fusion for GPS-Denied Navigation
dc.typeThesis
dc.date.updated2016-01-26T22:47:19Z
thesis.degree.departmentMechanical and Aerospace Engineering
thesis.degree.grantorThe University of Texas at Arlington
thesis.degree.levelDoctoral
thesis.degree.nameDoctor of Philosophy in Aerospace Engineering
dc.type.materialtext
dc.creator.orcid0000-0002-8235-3656


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