65 research outputs found

    P-RANSAC: An Integrity Monitoring Approach for GNSS Signal Degraded Scenario

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    Satellite navigation is critical in signal-degraded environments where signals are corrupted and GNSS systems do not guarantee an accurate and continuous positioning. In particular measurements in urban scenario are strongly affected by gross errors, degrading navigation solution; hence a quality check on the measurements, defined as RAIM, is important. Classical RAIM techniques work properly in case of single outlier but have to be modified to take into account the simultaneous presence of multiple outliers. This work is focused on the implementation of random sample consensus (RANSAC) algorithm, developed for computer vision tasks, in the GNSS context. This method is capable of detecting multiple satellite failures; it calculates position solutions based on subsets of four satellites and compares them with the pseudoranges of all the satellites not contributing to the solution. In this work, a modification to the original RANSAC method is proposed and an analysis of its performance is conducted, processing data collected in a static test

    A New Relative Receiver Autonomous Integrity Monitoring Algorithm for Multiple Failures

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    authors' final manuscriptIn near future, GNSS GPS modernization, renewed GLONASS and a new Galileo signal will be available. And the accuracy of position solution will be better by courtesy of improved quality of ranging signal. As an expected accuracy is better, the threshold for failure will be reduced. As a result, the prior probability of failures could be larger than what is used now. Due to the increased prior probability of failures, probability of simultaneous multiple failures cannot be neglected any more. Furthermore there will be many more ranging sources makes it necessary to consider the possibility of simultaneous multiple failures. This paper develops and analyzes a new Relative Receiver Autonomous Integrity Monitoring (RRAIM) algorithm which can treat no only a single failure but also simultaneous multiple failures. A proposed algorithm uses measurement residuals and satellite observation matrices of several consecutive epochs for Failure Detection and Exclusion (FDE). It detects failures by monitoring the error vector itself instead of monitoring the projection of the error vector. The simulation results show that the algorithm is able to detect any instance of multiple failures which are not detected by the conventional RAIM algorithm.OAIID:oai:osos.snu.ac.kr:snu2012-01/104/0000003405/18SEQ:18PERF_CD:SNU2012-01EVAL_ITEM_CD:104USER_ID:0000003405ADJUST_YN:NEMP_ID:A000360DEPT_CD:446CITE_RATE:0FILENAME:Manuscript_HoYun.pdfDEPT_NM:êž°êł„í•­êł”êł”í•™ë¶€EMAIL:[email protected]:

    Integrity Monitoring: From Airborne to Land Applications

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    Safety-critical applications in transportation require GNSS-based positioning with high levels of continuity, accuracy and integrity. The system needs to detect and exclude faults and to raise an alarm in the event of unsafe positioning. This capability is referred to as integrity monitoring (IM). While IM was considered until recently only in aviation, it is currently a key performance parameter in land applications, such as Intelligent Transport Systems (ITS). In this chapter the IM concepts, models and methods developed so far are compared. In particular, Fault Detection and Exclusion (FDE) and bounding of positioning errors methods borrowed from aviation (i.e. Weighted RAIM and ARAIM) are discussed in detail, in view of their possible adoption for land applications. Their strengths and limitations, and the modifications needed for application in the different context are highlighted. A practical demonstration of IM in ITS is presented

    Navigation Algorithm-Agnostic Integrity Monitoring based on Solution Separation with Constrained Computation Time and Sensor Noise Overbounding

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    Integrity monitoring (IM) in autonomous navigation has been extensively researched, but currently available solutions are mainly applicable to specific algorithms and sensors, or limited by linearity or 'Gaussianity' assumptions. This study investigates a Solution Separation (SS) based framework for universal IM, scalable to multi-sensor fusion as each hypothesis assumes a whole sensor measurement set as faulty. Architecturally we consider that: 1) multi sensor systems must account for various sensor noise models which lead to inconsistent estimates of uncertainties, 2) a module must be able to detect sensor failure or sensor noise mismodeling and suggest better bounds for the error, without being constantly conservative, 3) some algorithms are computationally heavy to monitor in the SS setting or the provided covariances cannot be interpreted in IM. A hybrid SS architecture can be practical, where some solutions are evaluated with a navigation algorithm with known characteristics, although the all-sensor-in solution is evaluated with the monitored algorithm. Experiments are run on filter and smoothing-based navigation algorithms. In addition, we experiment with hybrid SS monitoring and time-correlated noise to evaluate the appropriability of our framework in the context of the above-mentioned requirements. This is a novel framework in the IM domain, directly integrable in existing navigation solutions and, in our opinion, it will facilitate the quantification of the effect of different sensors in navigation safety.publishedVersio

    Integrity monitoring applied to the reception of GNSS signals in urban environments

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    L’intĂ©gritĂ© des signaux GNSS est dĂ©finie comme la mesure de la confiance qui peut ĂȘtre placĂ©e dans l’exactitude des informations fournies par le systĂšme de navigation. Bien que le concept d’intĂ©gritĂ© GNSS a Ă©tĂ© initialement dĂ©veloppĂ© dans le cadre de l’aviation civile comme une des exigences standardisĂ©es par l’Organisation de l’Aviation Civile Internationale (OACI) pour l’utilisation du GNSS dans les systĂšmes de Communication, Navigation, et Surveillance / ContrĂŽle du Trafic AĂ©rien (CNS/ATM), un large Ă©ventail d’applications non aĂ©ronautiques ont Ă©galement besoin de navigation par satellite fiable avec un niveau d’intĂ©gritĂ© garanti. Beaucoup de ces applications se situent en environnement urbain. Le contrĂŽle d’intĂ©gritĂ© GNSS est un Ă©lĂ©ment clĂ© des applications de sĂ©curitĂ© de la vie (SoL), telle que l’aviation, et des applications exigeant une fiabilitĂ© critique comme le tĂ©lĂ©pĂ©age basĂ© sur l’utilisation du GNSS, pour lesquels des erreurs de positionnement peuvent avoir des consĂ©quences juridiques ou Ă©conomiques. Chacune de ces applications a ses propres exigences et contraintes, de sorte que la technique de contrĂŽle d’intĂ©gritĂ© la plus appropriĂ©e varie d’une application Ă  l’autre. Cette thĂšse traite des systĂšmes de tĂ©lĂ©pĂ©age utilisant GNSS en environnement urbain. Les systĂšmes de navigation par satellite sont l’une des technologies que l’UE recommande pour le Service EuropĂ©en de TĂ©lĂ©pĂ©age Electronique (EETS). Ils sont dĂ©jĂ  en cours d’adoption: des systĂšmes de tĂ©lĂ©pĂ©age pour le transport poids lourd utilisant GPS comme technologie principale sont opĂ©rationnels en Allemagne et en Slovaquie, et un systĂšme similaire est envisagĂ© en France Ă  partir de 2013. À l’heure actuelle, le contrĂŽle d’intĂ©gritĂ© GPS s’appuie sur des systĂšmes dÂŽaugmentation (GBAS, SBAS, ABAS) conçus pour rĂ©pondre aux exigences de l’OACI pour les opĂ©rations aviation civile. CÂŽest la raison pour laquelle cette thĂšse dĂ©bute par une prĂ©sentation du concept d’intĂ©gritĂ© en aviation civile afin de comprendre les performances et contraintes des systĂšmes hĂ©ritĂ©s. La thĂšse se poursuit par une analyse approfondie des systĂšmes de tĂ©lĂ©pĂ©age et de navigation GNSS en milieu urbain qui permets de dĂ©river les techniques de contrĂŽle d’intĂ©gritĂ© GNSS les plus adaptĂ©es. Les algorithmes autonomes de type RAIM ont Ă©tĂ© choisis en raison de leur souplesse et leur capacitĂ© dÂŽadaptabilitĂ© aux environnements urbains. Par la suite, le modĂšle de mesure de pseudodistances est Ă©laborĂ©. Ce modĂšle traduit les imprĂ©cisions des modĂšles de correction des erreurs d’horloge et d’ephemeride, des retards ionosphĂ©riques et troposphĂ©riques, ainsi que le bruit thermique rĂ©cepteur et les erreurs dues aux multitrajets. Les exigences d’intĂ©gritĂ© GNSS pour l’application tĂ©lĂ©pĂ©age sont ensuite dĂ©rivĂ©es Ă  partir de la relation entre les erreurs de positionnement et leur effets dans la facturation finale. Deux algorithmes RAIM sont alors proposĂ©s pour l’application pĂ©age routier. Le premier est l’algorithme basĂ© sur les rĂ©sidus de la solution des moindres carrĂ©s pondĂ©rĂ©s (RAIM WLSR), largement utilisĂ© dans l’aviation civile. Seulement, un des principaux dĂ©fis de l’utilisation des algorithmes RAIM classiques en milieux urbains est un taux Ă©levĂ© d’indisponibilitĂ© causĂ© par la mauvaise gĂ©omĂ©trie entre le rĂ©cepteur et les satellites. C’est pour cela que un nouvel algorithme RAIM est proposĂ©. Cet algorithme, basĂ© sur le RAIM WLSR, est conçu de sorte Ă  maximiser l’occurrence de fournir un positionnement intĂšgre dans un contexte tĂ©lĂ©pĂ©age. Les performances des deux algorithmes RAIM proposĂ©s et des systĂšmes de tĂ©lĂ©pĂ©age associĂ©s sont analysĂ©s par simulation dans diffĂ©rents environnements ruraux et urbains. Dans tous les cas, la disponibilitĂ© du nouvel RAIM est supĂ©rieure Ă  celle du RAIM WLSR. ABSTRACT : Global Navigation Satellite Systems (GNSS) integrity is defined as a measure of the trust that can be placed in the correctness of the information supplied by the navigation system. Although the concept of GNSS integrity has been originally developed in the civil aviation framework as part of the International Civil Aviation Organization (ICAO) requirements for using GNSS in the Communications, Navigation, and Surveillance / Air Traffic Management (CNS/ATM) system, a wide range of non-aviation applications need reliable GNSS navigation with integrity, many of them in urban environments. GNSS integrity monitoring is a key component in Safety of Life (SoL) applications such as aviation, and in the so-called liability critical applications like GNSS-based electronic toll collection, in which positioning errors may have negative legal or economic consequences. At present, GPS integrity monitoring relies on different augmentation systems (GBAS, SBAS, ABAS) that have been conceived to meet the ICAO requirements in civil aviation operations. For this reason, the use of integrity monitoring techniques and systems inherited from civil aviation in non-aviation applications needs to be analyzed, especially in urban environments, which are frequently more challenging than typical aviation environments. Each application has its own requirements and constraints, so the most suitable integrity monitoring technique varies from one application to another. This work focuses on Electronic Toll Collection (ETC) systems based on GNSS in urban environments. Satellite navigation is one of the technologies the directive 2004/52/EC recommends for the European Electronic Toll Service (EETS), and it is already being adopted: toll systems for freight transport that use GPS as primary technology are operational in Germany and Slovakia, and France envisages to establish a similar system from 2013. This dissertation begins presenting first the concept of integrity in civil aviation in order to understand the objectives and constraints of existing GNSS integrity monitoring systems. A thorough analysis of GNSS-based ETC systems and of GNSS navigation in urban environments is done afterwards with the aim of identifying the most suitable road toll schemes, GNSS receiver configurations and integrity monitoring mechanisms. Receiver autonomous integrity monitoring (RAIM) is chosen among other integrity monitoring systems due to its design flexibility and adaptability to urban environments. A nominal pseudorange measurement model suitable for integrity-driven applications in urban environments has been calculated dividing the total pseudorange error into five independent error sources which can be modelled independently: broadcasted satellite clock corrections and ephemeris errors, ionospheric delay, tropospheric delay, receiver thermal noise (plus interferences) and multipath. In this work the fault model that includes all non-nominal errors consists only of major service failures. Afterwards, the GNSS integrity requirements are derived from the relationship between positioning failures and toll charging errors. Two RAIM algorithms are studied. The first of them is the Weighted Least Squares Residual (WLSR) RAIM, widely used in civil aviation and usually set as the reference against which other RAIM techniques are compared. One of the main challenges of RAIM algorithms in urban environments is the high unavailability rate because of the bad user/satellite geometry. For this reason a new RAIM based on the WLSR is proposed, with the objective of providing a trade-off between the false alarm probability and the RAIM availability in order to maximize the probability that the RAIM declares valid a fault-free position. Finally, simulations have been carried out to study the performance of the different RAIM and ETC systems in rural and urban environments. In all cases, the availability obtained with the novel RAIM improve those of the standard WLSR RAIM
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