The goal of this thesis is a complete design and realization of a device that is able to communicate with GPS module iTrax300 and display the coordinates received from the module. The thesis deals with the GPS, localization principles and the standard communication protocol for navigation systems - the NMEA 0183 protocol. Futhermore it is dealing with the particular steps in the realization of the engineered device (from the specification of requirements at the beginning to the testing of its functionality in the end). The GPS coordinates, the Coordinated Universal Time (UTC), the date, the altitude and the speed on the ground can be displayed. There is also a possibility to put in any coordinates, the direction and the distance to the point are displayed afterwards. The device enables the track storage in the memory as well. The track is viewable while connecting the device and the PC through the USB interface.

The aim of this thesis is to innovate NCL 07 unit made by NAM system a.s. The new device is intended to have improved parameters and diminished dimensions. It should be fully comparable to similar products on market. In the first part there are described features and individual circuits of NCL07 unit. Further there is done an analysis to suggest modifications leading to reduce proportions of DPS and to enhance other parameters including SW design improvement. Theoretical part deals with selection of main measured values and methods of verification of measurement accuracy. There is also described theoretical basis used in the oncoming sections of the thesis. In the practical part there are presented procedures of designs of innovated product. In the conclusion there will be made testing of new unit and results will be compared to competitive commodities.

RF receiver improvements in size, weight, power, and sensitivity are constant goals in the wireless communications community. The combination of phased array antenna systems with high speed analog to digital converters helps engineers meet these goals, because many of the analog components and tasks found in a traditional receive chain are moved into the digital domain. Although the hard work of signal reception is moved into digital signal processing, digital receivers rely on a high performance analog front end to properly condition a signal before analog to digital conversion. In this thesis, two RF front ends are developed for direct sampling L-band phased array receiver applications, which comprise the two main chapters of this document. Both RF front ends are developed on low cost, quick turnaround time PCB materials. Results for system gain and noise figure are presented for each front end. First, the development of an L-band analog front end for a direct sampling GPS phased array receiver is described, with particular attention to gain and noise figure in context of the full system link budget. The RF front end for the GPS phased array receiver meets design expectations by achieving a system gain of 65 dB and a system noise figure of 1.5 dB at the GPS L1 frequency. Second, the redesign and improvement of the Advanced L-band Phased Array Camera (ALPACA) RF over fiber transmitter is documented. New mechanical and electrical design requirements were brought on from the change of target observatory from the collapsed Arecibo obervatory in Puerto Rico, to the Greenbank Observatory in Greenbank, West Virginia. The ALPACA RF over fiber signal transport system with the redesigned transmitter reaches the design expectation of a system noise temperature contribution less than 1 K. Average gain of the RF over fiber system is 49 dB, gain differences between channels are less than 2 dB, and isolation between channels is better than 35 dB. Under optimal conditions, the noise figure of the RF over fiber link is 2.4 dB (213.3 K), which allows for up to 11 dB of attenuation to be added to any given transmit channel to level the gain across all 138 ALPACA channels.

La navigation avec les systèmes de navigation par satellites (GNSS) est un réel défi dans des environnements contraints (semi-urbain, urbain, feuillage dense) à cause des multitrajets et du masquage du signal. Cette thèse propose un nombre de solutions architecturales et algorithmiques pour le récepteur GNSS afin de pallier ces problèmes. Ces solutions se veulent capables d’exploiter les atouts des poursuites scalaire et vectorielle tout en minimisant leurs défauts et de profiter de l’efficacité de certaines techniques de filtrage Bayésien non linéaire quant à aborder la non-Gaussianité et les non-linéarités associées au problème de navigation et de poursuite vectorielle. Une attention particulière est accordée à certains estimateurs Bayésiens qui essaient d’approximer la loi a posteriori sans linéariser le modèle de filtrage, notamment le filtre de Kalman et les méthodes de filtrage particulaire, mais aussi au filtre de Kalman étendu, dont l’estimation de la loi a posteriori est basée sur la linéarisation du modèle de filtrage. En premier lieu, une brève étude bibliographique présentant les fondamentaux des systèmes et des récepteurs GNSS ainsi que les algorithmes de navigation et de poursuite y associés est faite. Ensuite le fonctionnement d’un récepteur GNSS en milieux contraints est investigué. La thèse propose des modèles pour caractériser les erreurs de poursuite induites par les multitrajets dans une boucle de poursuite vectorielle. Ces modèles permettent d’exprimer les erreurs de poursuite en fonction du délai, de la phase et de la fréquence d’évanouissement des multitrajets. En exploitant le fait que la présence des multitrajets se reflète sur la sortie moins des corrélateurs, de nouveaux détecteurs de multitrajets sont formulés. Un détecteur de masquage du signal direct est aussi proposé. L’attention se tourne ensuite vers la conception d’architectures robustes de poursuite et positionnement pour un récepteur GNSS, incorporant les détecteurs proposés et d’autres indicateurs de qualité. Une boucle de poursuite vectorielle capable de détecter et d’exclure des mesures qui ne sont pas saines du calcul de la solution de navigation en utilisant les indicateurs de qualité est proposée. Deux autres boucles de poursuite, la boucle de poursuite adaptative scalaire-vectorielle et la boucle de poursuite conjointe scalaire-vectorielle, avec la même capacité de détection et exclusion de fautes, sont formulées. Elles bénéficient de la robustesse de la poursuite vectorielle en milieux contraints et de la précision de la poursuite scalaire en milieux dégagés. Des résultats expérimentaux montrent que les solutions conçues offrent une meilleure alternative de poursuite et positionnement par rapport aux boucles usuelles de poursuite scalaire et de poursuite vectorielle. Enfin, la thèse présente des approches de filtrage Bayésien non linéaire pour résoudre le problème de navigation et de poursuite vectorielle. Des stratégies de filtrage itératives et adaptatives appliquées au filtre de Kalman sont étudiées. Une nouvelle approche de filtrage particulaire dénommée filtre particulaire itératif et adaptatif (IAUPF) est formulée. Cette approche exploite les propriétés de convergence des méthodes itératives, l’immunité à la divergence dont jouissent les filtres adaptatifs, et la synergie entre les approches de filtrage particulaire et de Kalman. Des simulations de Monte Carlo avec une borne inférieure de Cramér-Rao a posteriori comme référence ainsi que des résultats expérimentaux montrent que l’approche IAUPF a une meilleure performance comparativement aux autres estimateurs Bayésiens présentés / Navigation with Global Navigation Satellite Systems (GNSS) is a real challenge in harsh environments (suburban, urban, heavy foliage) due to multipath and signal blockage. This thesis proposes a number of GNSS receiver architectural and algorithmic solutions to deal with this challenge. These solutions aim at exploiting the strengths of scalar and vector tracking while minimizing their weaknesses and at utilizing the efficiency of some nonlinear Bayesian filtering techniques in addressing the nonlinearities and non-Gaussianities associated with the navigation and vector tracking problem. Attention is given to some Bayesian estimators that approximate the posterior distribution without linearizing the filtering model, namely the unscented Kalman and particle filtering methods, as well as to the extended Kalman filter, whose posterior estimation is grounded on linearization of the filtering model.First, a brief literature review that presents the fundamentals of GNSS and GNSS receivers together with the applied navigation and tracking algorithms is provided. Then an investigation of the GNSS receiver operation in multipath environments is performed. The thesis proposes models for characterizing multipath induced tracking errors in a vector tracking loop. These models make it possible to express the tracking errors with respect to multipath delay, multipath phase and multipath fading frequency. By exploiting the fact that multipath presence is mirrored on the Early-minus-Late correlator output, novel multipath detectors are devised. A correlator-based non-line-of-sight detector is designed as well. Attention is then directed towards the design of robust tracking and positioning GNSS receiver architectures that incorporate the proposed detectors among other signal quality indicators. A vector tracking scheme capable of detecting and excluding unhealthy measurements from position-velocity-time calculation in the navigator using correlator-based signal quality indicators is suggested. Two other novel tracking schemes, the adaptive scalar-vector tracking loop and the conjoint scalar-vector tracking loop, with the same fault detection and exclusion capability, are formulated. They benefit from vector tracking robustness in harsh environments and scalar tracking positioning accuracy in open sky environments. Experimental results show that the proposed solutions have better tracking and positioning performance than the usual scalar and vector tracking loops. Finally, the thesis presents a number of nonlinear Bayesian filtering approaches to solve the navigation and vector tracking problem. Iterative and adaptive strategies as applied to the unscented Kalman filter are studied. A novel unscented particle filter approach, the iterated adaptive unscented particle filter (IAUPF), is proposed. This approach exploits the convergence properties of iterative methods, the divergence suppression benefits of adaptive filters and the synergy of unscented Kalman and particle filtering approaches. Monte-Carlo simulations conducted with a posterior Cramér-Rao lower bound used as benchmarking reference as well as experimental results demonstrate that the IAUPF outperforms the other Bayesian estimators that are presented

No description available.

The thesis contains complete design of complex system for acquisition of data from bus of a vehicle. It resolves problems of connection of a new node to CAN bus of a vehicle, communication protocol NMEA 0183 of GPS receivers, logging of caught CAN frames into database system MySQL, and proposes algorithms of application for operation of the system. It includes also process of complete installation based on established concept and test results of the system in real situations.

No description available.

A software GPS receiver is a functional GPS receiver in software. It has several advantages compared to its hardware counterparts. For instance, improvements in receiver architecture as well as GPS system structure can be easily adapted to it. Furthermore, interaction between nearby sensors can be coordinated easily. In this thesis, a SGR (software GPS receiver) is presented from a practical point of view. Major components of the SGR are implemented in Matlab environment. Furthermore, some alternative algorithms are implemented. SGR implementation is considered in two main sections namely a signal processing section and a navigation section. Signal processing section is driven by the raw GPS signal samples obtained from a GPS front-end of NordNavTM R-25 instrument. The conventional and the block adjustment of synchronizing signal (BAAS) processing methods are implemented and their performances are compared in terms of their speed and outputs. Signal processing section outputs raw GPS measurements and navigation data bits. Since the output data length is insufficient in our case, navigation section input is fed from AshtechTM GPS receiver for a moving platform and TrimbleTM GPS Receiver for a stationary platform. Satellite position computation, pseudorange corrections, Kalman filter and LSE (least squares estimation) are implemented in the navigation section. Kalman filter and LSE methods are compared in terms of positioning accuracy for a moving as well as a stationary platform. Results are compared with the commercial GPS outputs. This comparison shows that the software navigation section is equivalent to the commercial GPS in terms of positioning accuracy.

Made available in DSpace on 2014-12-17T14:55:41Z (GMT). No. of bitstreams: 1 GlaubertoLAA.pdf: 3487440 bytes, checksum: bcd5cef1c854f4d01f9c73419e1d7d42 (MD5) Previous issue date: 2009-11-20 / Global Positioning System, or simply GPS, it is a radionavigation system developed by United States for military applications, but it becames very useful for civilian using. In the last decades Brazil has developed sounding rockets and today many projects to build micro and nanosatellites has appeared. This kind of vehicles named spacecrafts or high dynamic vehicles, can use GPS for its autonome location and trajectories controls. Despite of a huge number of GPS receivers available for civilian applications, they cannot used in high dynamic vehicles due environmental issues (vibrations, temperatures, etc.) or imposed dynamic working limits. Only a few nations have the technology to build GPS receivers for spacecrafts or high dynamic vehicles is available and they imposes rules who difficult the access to this receivers. This project intends to build a GPS receiver, to install them in a payload of a sounding rocket and data collecting to verify its correct operation when at the flight conditions. The inner software to this receiver was available in source code and it was tested in a software development platform named GPS Architect. Many organizations cooperated to support this project: AEB, UFRN, IAE, INPE e CLBI. After many phases: defining working conditions, choice and searching electronic, the making of the printed boards, assembling and assembling tests; the receiver was installed in a VS30 sounding rocket launched at Centro de Lan?amento da Barreira do Inferno in Natal/RN. Despite of the fact the locations data from the receiver were collected only the first 70 seconds of flight, this data confirms the correct operation of the receiver by the comparison between its positioning data and the the trajectory data from CLBI s tracking radar named ADOUR / O Sistema de Posicionamento Global, conhecido mundialmente pala sigla GPS, ? um sistema de radionavega??o constru?do pelos norte-americanos com inten??es militares, mas que encontraram, com o passar do tempo, muitas aplica??es de uso civil. No Brasil, al?m do desenvolvimento de foguetes de sondagem, come?am a aparecer projetos de constru??o de micro e nanosat?lites. Estes ve?culos denominados espaciais ou de alta din?mica podem, quando em voo, usufruir do sistema GPS para localiza??o aut?noma e verifica??o/controle das suas trajet?rias. Apesar da enorme disponibilidade de receptores GPS no mercado civil, estes n?o podem ser utilizados em ve?culos de alta din?mica, seja por quest?es ambientais (vibra??es, temperaturas elevadas, etc.) ou por prote??o l?gica (via software). Os receptores para uso em ve?culos de alta din?mica, ou ve?culos espaciais, fazem parte de uma tecnologia restrita a poucos pa?ses, que estabelecem regras muito r?gidas para suas aquisi??es. O presente projeto objetiva construir e validar funcionamento b?sico deste receptor ao instal?-lo num foguete de sondagem e coleta de dados em voo. O software a ser utilizado no receptor j? estava dispon?vel em c?digo fonte e testado em uma plataforma de desenvolvimento denominada GPS Architect. V?rios organismos cooperaram para realiza??o projeto: AEB, UFRN, IAE, INPE e CLBI. Ap?s v?rios passos para realiza??o do projeto: defini??o das condi??es de funcionamento, escolha e aquisi??o dos componentes eletr?nicos, fabrica??o das placas de circuito impresso, montagem e testes de integra??o; o mesmo foi instalado num foguete de sondagem VS30 lan?ado a partir do Centro de Lan?amento da Barreira do Inferno em Natal/RN. Apesar da coleta parcial dos dados do receptor, por falha t?cnica do sistema de telemetria do foguete, os resultados obtidos foram suficientes para validar o funcionamento do receptor a partir da compara??o entre os dados de trajetografia fornecidos pelo receptor GPS e o radar de trajetografia do CLBI conhecido como Radar ADOUR

Made available in DSpace on 2014-12-17T14:55:58Z (GMT). No. of bitstreams: 1 TullioEMR_DISSERT.pdf: 2349636 bytes, checksum: 1b35ab0d9433bcc6b9750162da2fd889 (MD5) Previous issue date: 2011-03-25 / Spacecraft move with high speeds and suffer abrupt changes in acceleration. So, an onboard GPS receiver could calculate navigation solutions if the Doppler effect is taken into consideration during the satellite signals acquisition and tracking. Thus, for the receiver subject to such dynamic cope these shifts in the frequency signal, resulting from this effect, it is imperative to adjust its acquisition bandwidth and increase its tracking loop to a higher order. This paper presents the changes in the GPS Orion s software, an open architecture receiver produced by GEC Plessey Semiconductors, nowadays Zarlink, in order to make it able to generate navigation fix for vehicle under high dynamics, especially Low Earth Orbit satellites. GPS Architect development system, sold by the same company, supported the modifications. Furthermore, it presents GPS Monitor Aerospace s characteristics, a computational tool developed for monitoring navigation fix calculated by the GPS receiver, through graphics. Although it was not possible to simulate the software modifications implemented in the receiver in high dynamics, it was observed that the receiver worked in stationary tests, verified also in the new interface. This work also presents the results of GPS Receiver for Aerospace Applications experiment, achieved with the receiver s participation in a suborbital mission, Operation Maracati 2, in December 2010, using a digital second order carrier tracking loop. Despite an incident moments before the launch have hindered the effective navigation of the receiver, it was observed that the experiment worked properly, acquiring new satellites and tracking them during the VSB-30 rocket flight. / Ve?culos espaciais se movem com velocidades elevadas e sofrem mudan?as bruscas de acelera??o. Ent?o, para que um receptor de GPS possa calcular solu??es de navega??o estando a bordo de tais ve?culos, o efeito Doppler deve ser levado em considera??o durante os processos de aquisi??o e rastreio de sinais de sat?lites. Assim, para que o receptor submetido ? alta din?mica comporte os deslocamentos de frequ?ncia no sinal recebido, decorrentes desse efeito, ? necess?rio ajustar sua largura de banda de varredura de frequ?ncias e aumentar a ordem de sua malha de rastreio. Este trabalho apresenta as modifica??es no software no GPS Orion, um receptor de arquitetura aberta da GEC Plessey Semiconductors, hoje Zarlink, a fim de torn?-lo apto a gerar solu??es de navega??o em ve?culos submetidos ? alta din?mica, especialmente sat?lites de ?rbita baixa. A plataforma de desenvolvimento GPS Architect, comercializada pela mesma empresa, foi utilizada para dar suporte ?s modifica??es. Al?m disso, s?o apresentadas as caracter?sticas do Monitor GPS Aeroespacial, uma ferramenta computacional desenvolvida para monitorar as solu??es de navega??o calculadas pelo receptor de GPS atrav?s de gr?ficos. Apesar de n?o ter sido poss?vel fazer simula??es em alta din?mica com as modifica??es de software implementadas no receptor, verificou-se seu funcionamento satisfat?rio, em regime estacion?rio, fazendo uso, inclusive, da nova interface gr?fica. A disserta??o apresenta ainda os resultados do experimento Receptor de GPS para Aplica??es Aeroespaciais, obtidos com a participa??o do receptor numa miss?o suborbital, a Opera??o Maracati 2, em dezembro de 2010, utilizando uma malha de rastreio de portadora digital de segunda ordem. Apesar de um incidente ocorrido momentos antes do lan?amento ter prejudicado a navega??o efetiva do receptor, foi observado que o experimento funcionou adequadamente, rastreando e adquirindo novos sat?lites durante o voo do foguete VSB-30.