Overbounding non-zero mean Gaussian ranging error for navigation integrity of LAAS
Navigation integrity is one of the most critical elements in the development of Local Area Augmentation System (LAAS) architecture and remains an unsolved key technical problem. For example, in LAAS, the navigation integrity is ensured through the computation of the aircraft position error bounds (i...
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description | Navigation integrity is one of the most critical elements in the development of Local Area Augmentation System (LAAS) architecture and remains an unsolved key technical problem. For example, in LAAS, the navigation integrity is ensured through the computation of the aircraft position error bounds (i.e., Protection Levels, VPL/LPL) in which implicitly Zero-mean, normally distributed fault free error models are assumed. However, it is observed that true ranging error involved biases. For example, significant values of mean, in satellites ranging error, extracted from LAAS Test Prototype (LTP) data for ten satellites. Therefore, to ensure navigation integrity of LAAS, such true mean error in ranging must be bounded with zero-mean normal distribution. In our past work, theoretical bounds were generated and negligibility of mean was sought within Alert Limits. In this paper, these bounds are reexamined and quantified by using true mean values and also considering availability. In this regard, both simulation and experimental data are heavily used for forming inflations on broadcast sigma to bound and accommodate ranging mean error effects. |
doi_str_mv | 10.1109/RAST.2005.1512601 |
format | Conference Proceeding |
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For example, in LAAS, the navigation integrity is ensured through the computation of the aircraft position error bounds (i.e., Protection Levels, VPL/LPL) in which implicitly Zero-mean, normally distributed fault free error models are assumed. However, it is observed that true ranging error involved biases. For example, significant values of mean, in satellites ranging error, extracted from LAAS Test Prototype (LTP) data for ten satellites. Therefore, to ensure navigation integrity of LAAS, such true mean error in ranging must be bounded with zero-mean normal distribution. In our past work, theoretical bounds were generated and negligibility of mean was sought within Alert Limits. In this paper, these bounds are reexamined and quantified by using true mean values and also considering availability. In this regard, both simulation and experimental data are heavily used for forming inflations on broadcast sigma to bound and accommodate ranging mean error effects.</description><identifier>ISBN: 9780780389779</identifier><identifier>ISBN: 0780389778</identifier><identifier>DOI: 10.1109/RAST.2005.1512601</identifier><language>eng</language><publisher>IEEE</publisher><subject>Aircraft navigation ; Computer architecture ; Data mining ; Distributed computing ; Gaussian distribution ; Protection ; Prototypes ; Satellite broadcasting ; Satellite navigation systems ; Testing</subject><ispartof>Proceedings of 2nd International Conference on Recent Advances in Space Technologies, 2005. 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In this paper, these bounds are reexamined and quantified by using true mean values and also considering availability. In this regard, both simulation and experimental data are heavily used for forming inflations on broadcast sigma to bound and accommodate ranging mean error effects.</description><subject>Aircraft navigation</subject><subject>Computer architecture</subject><subject>Data mining</subject><subject>Distributed computing</subject><subject>Gaussian distribution</subject><subject>Protection</subject><subject>Prototypes</subject><subject>Satellite broadcasting</subject><subject>Satellite navigation systems</subject><subject>Testing</subject><isbn>9780780389779</isbn><isbn>0780389778</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2005</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotUEFqwzAQFJRCS5oHlF506s2uJFu2dDShTQOBQJK7Wasro5JIqWQH0tfXJRl2mYUZhmUIeeYs55zpt22z2-eCMZlzyUXF-B2Z61qxaQql61o_kHlK32xCoSumykey3ZwxdmH0X8731Aef_WIM9Ijg6RLGlNx0RPD9v4wxhkjttB7OrofBBU-dH7CPbrjQYOm6aXZP5N7CIeH8xjOy_3jfLz6z9Wa5WjTrzAlWDZkyymKpDetKYbWcnoRCoRAG6rqqhJTWcg5WSWY7QKNRWJS1MQDGoLTFjLxeY08x_IyYhvboksHDATyGMbVCM13yQk3Gl6vRIWJ7iu4I8dLeGir-AOd9XTw</recordid><startdate>2005</startdate><enddate>2005</enddate><creator>Sayim, I.</creator><creator>Pervan, B.</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope><scope>7TB</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>2005</creationdate><title>Overbounding non-zero mean Gaussian ranging error for navigation integrity of LAAS</title><author>Sayim, I. ; Pervan, B.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i206t-8c8fe49c0b42f95078a38e22ca7766255ff11af850fbaec9e2fe57ccaacce5f3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2005</creationdate><topic>Aircraft navigation</topic><topic>Computer architecture</topic><topic>Data mining</topic><topic>Distributed computing</topic><topic>Gaussian distribution</topic><topic>Protection</topic><topic>Prototypes</topic><topic>Satellite broadcasting</topic><topic>Satellite navigation systems</topic><topic>Testing</topic><toplevel>online_resources</toplevel><creatorcontrib>Sayim, I.</creatorcontrib><creatorcontrib>Pervan, B.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Sayim, I.</au><au>Pervan, B.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Overbounding non-zero mean Gaussian ranging error for navigation integrity of LAAS</atitle><btitle>Proceedings of 2nd International Conference on Recent Advances in Space Technologies, 2005. 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In our past work, theoretical bounds were generated and negligibility of mean was sought within Alert Limits. In this paper, these bounds are reexamined and quantified by using true mean values and also considering availability. In this regard, both simulation and experimental data are heavily used for forming inflations on broadcast sigma to bound and accommodate ranging mean error effects.</abstract><pub>IEEE</pub><doi>10.1109/RAST.2005.1512601</doi><tpages>7</tpages></addata></record> |
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subjects | Aircraft navigation Computer architecture Data mining Distributed computing Gaussian distribution Protection Prototypes Satellite broadcasting Satellite navigation systems Testing |
title | Overbounding non-zero mean Gaussian ranging error for navigation integrity of LAAS |
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