Dissertations / Theses on the topic 'Autonomous satellites'
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Anderson, Jason Lionel. "Autonomous Satellite Operations For CubeSat Satellites." DigitalCommons@CalPoly, 2010. https://digitalcommons.calpoly.edu/theses/256.
Full textSantiago, Luis. "AUTONOMOUS CONTROLS ALGORITHMFOR FORMATION FLYING OF SATELLITES." Master's thesis, University of Central Florida, 2006. http://digital.library.ucf.edu/cdm/ref/collection/ETD/id/2641.
Full textM.S.
Department of Mechanical, Materials and Aerospace Engineering;
Engineering and Computer Science
Aerospace Engineering
Badger, Stanley. "Autonomous detection, navigation, and propulsion for satellites." Kansas State University, 2009. http://hdl.handle.net/2097/1402.
Full textDepartment of Electrical and Computer Engineering
William B. Kuhn
With the increasing number of satellites and space debris in all orbits the need for individual satellites to be able to autonomously detect and determine methods to navigate around them is increasing. Even with continued input and control from a ground station, the ability for a satellite to act to save itself from obstacles not visible from ground stations, or if communications were temporarily lost could be key to saving millions of dollars in hardware as well as improving overall performance and operational lifetimes.
Ruiz-de-Azua, Ortega Joan Adrià. "Contribution to the development of autonomous satellite communications networks : the internet of satellites." Doctoral thesis, Universitat Politècnica de Catalunya, 2020. http://hdl.handle.net/10803/671780.
Full textL'espai esta experimentant! una revolució degut a l'aparició de serveis per satèl·lit que satisfan les noves demandes ambientals, socials i geo-polítiques. Els sistemes de satèl·lits per observar la Terra han esdevingut recursos essencials per el control del clima, !'agricultura moderna, i altres aplicacions. L'entrada del 5G en el sector aeroespacial ha promogut els satèl·lits com plataformes per aconseguir una cobertura global. Aquestes necessitats poden ser classificades en dos requeriments de sistema: (1) L'augment de la capacitat per transferir dades, i (2) la reducció de la latència en les comunicacions d'extrem-a-extrem. Els sistemes distribuïts de satèl·lits han esdevingut una solució efectiva amb múltiples satèl·lits essent operats simultàniament per satisfer uns requeriments comuns. Els sistemes federats de satèl·lits són candidats prometedors per explotar el potencial de les arquitectures distribuïdes mitjançant col·laboracions oportunistiques entre satèl·lits per compartir recursos. Aquestes col·laboracions, anomenades federacions, permeten concebre l'espai com un entorn on els satèl·lits poden beneficiar-se dels recursos d'altres per millorar el seu funcionament. Les investigacions s'han central en desenvolupar noves tecnologies per aquestes federacions. No obstant, molts aspectes de disseny encara són punts oberts de recerca, com ara el desenvolupament de protocols de comunicació per establir aquestes federacions. Aquesta tesina contribueix definint mecanismes que permeten desplegar una infraestructura en xarxa per establir federacions. A més a més, es discuteix sobre aquest context interconnectat on els satèl·lits poden establir esporàdicament i oportunísticament les federacions. Aquest escenari s'ha anomenat la Internet dels Satèl·lits, i promou els desplegament temporal de xarxes entre satèl·lits heterogenis. Aquesta característica, amb el moviment dels satèl·lits, suposa un repte en la definició de rutes entre extrems formades per satèl·lits intermitjos. Una revisió de protocols d'enrutament actuals d'altres xarxes de satèl·lits s'ha realitzat per identificar el protocol ideal per aquest tipus de xarxa dinàmica. El resultat remarca la necessitat de combinar capacitats de diferents dom in is per aconseguir el funcionament desitjat. Entre aquestes, la capacitat de preveure futurs enllaços entre satèl·lits esdevé crucial per mitigar la fragmentació de la xarxa. Amb aquesta premissa, aquesta tesina presenta un protocol predictiu que estima aquests contactes entre satèl·lits de forma distribuïda. Aquesta nova capacitat pot complementar el protocol d'enrutament mitjançant l'estimació de futures rutes com seqüències of contactes de satèl·lits a través del temps. La recerca presentada en aquesta tesina també respon altres preguntes que no s'havien res post encara: Com els satèl·lits poden descobrir els recursos disponibles en la xarxa? Quins són els mecanismes necessaris per establir i mantenir una federació? Una pila de protocols per cobrir aquesta necessitat tecnològica ha sigut desenvolupat. El protocol de dispersió de la disponibilitat de serveis oportunístics permet notificar els serveis disponibles en un satèl·lit, mentre que el protocol desplegament i control de federacions s'encarrega d'establir i gestionar les federacions. L'aplicació d'aquests protocols considerablement van realçar la capacita! del sistema de satèl·lit per descarregar dades, esdevenint així potenciadors de futures missions. Aquests resultats han motivat el desenvolupament d'un sistema dedica!, que inclou un dispositiu de comunicacions per crear enllaços entre satèl·lit. Aquest sistema ha estat verifica! en una campanya de globus estratosfèrics, i ha sigut integral en una missió de CubeSats. Aquesta dissertació presenta els resultats de la campanya, els quals emfasitzen els profits i viabilitat d'aquesta implementació.
Salazar, Kardozo Alexandros. "A High-Level Framework for the Autonomous Refueling of Satellite Constellations." Thesis, Georgia Institute of Technology, 2007. http://hdl.handle.net/1853/14534.
Full textMartinson, Nicholas S. "Obstacle avoidance guidance and control for autonomous satellites." [Gainesville, Fla.] : University of Florida, 2009. http://purl.fcla.edu/fcla/etd/UFE0041033.
Full textHashida, Yoshikazu. "Analytical solution for autonomous determination of near circular orbits." Thesis, University of Surrey, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.274353.
Full textAorpimai, Manop. "Low-thrust orbit control of LEO small satellites." Thesis, University of Surrey, 2000. http://epubs.surrey.ac.uk/843024/.
Full textNagarajan, N. "Autonomous Orbit Estimation For Near Earth Satellites Using Horizon Scanners." Thesis, Indian Institute of Science, 1994. http://hdl.handle.net/2005/155.
Full textRamos, Bosch Pedro. "Improvements in autonomous GPS navigation of Low Earth Orbit satellites." Doctoral thesis, Universitat Politècnica de Catalunya, 2008. http://hdl.handle.net/10803/7019.
Full textAquesta rang d'alçades fa que els LEO siguin utilitzats per un ampli rang d'aplicacions, com a repetidors de comunicacions, sensors remots, determinació gravimètrica i magnetomètrica, altimetria oceànica, determinació atmosfèrica i en operacions de Search and Rescue (Cerca i rescat). El seu posicionament precís és de gran importància per a poder complir correctament amb els seus objectius. En aquest sentit, una gran quantitat de satèl·lits LEO tenen un receptor GPS, que permet fer mesures GPS durant tot el seu recorregut al voltant de la Terra. Aquestes mesures poden ser utilitzades per determinar la trajectòria del satèl·lit. Aquesta operació es fa normalment a terra, després que el satèl·lit hagi transmès totes les mesures que ha pres. La capacitat de fer aquest posicionament en temps real a bord del satèl·lit és una necessitat per algunes aplicacions. El posicionament autònom es molt diferent del que es pot fer a terra, ja que el processador del satèl·lit te grans limitacions en recursos computacionals, per tant els complexos models i càlculs fets en un ordinador normal a terra, son completament excessius per un ordinador espacial. A més, alguns dels models utilitzats en l'estimació de la trajectòria necessiten dades addicionals (com activitat solar, o paràmetres de rotació de la Terra) que no son disponibles en temps real, per tant s'han de fer algunes aproximacions per tal de no necessitar cap d'aquestes dades. Aquesta tesis estudiarà la navegació autònoma amb GPS de satèl·lits LEO, tendència que esta incrementant la seva importància per les aplicacions tan científiques com tecnològiques que se'n poden derivar. La tesi desenvoluparà nous algoritmes i mètodes per obtenir una posició acurada i continua per LEOs. S'han cobert diferent aspectes:
· Mitigació de multipath e interferències. Les reflexions de senyals GPS en l'estructura del satèl·lit crea una distorsió que afecta la distància mesurada. La repetibilitat d'aquests efectes en relació amb l'orientació del satèl·lit pot ser utilitzat per a mitigar el seu impacte en la solució de navegació. S'han desenvolupat tècniques de mitigació de multipath i interferències per receptors d'una i de dos freqüències.
· Models dinàmics de forces. L'alta predictibilitat de la trajectòria d'objectes orbitant la Terra pot ser utilitzat en sinergia amb el GPS per a aconseguir solucions més precises que fent servir únicament GPS. Això s'utilitza normalment en estratègies en postprocess, però te grans requeriments computacionals, i necessita paràmetres no disponibles en temps real. La simplificació d'aquests models, i la supressió de paràmetres no disponibles es necessari per poder aplicar aquesta tècnica de processat en condicions de temps real.
· Maniobres. Els cossos en òrbita al voltant de la Terra no segueixen una trajectòria perfectament predeible. Hi han petites pertorbacions que modifiquen la seva trajectòria a llarg termini, i a més, el fregament atmosfèric frena poc a poc al satèl·lit, disminuint la seva alçada. Això fa necessari una correcció periòdica de la seva trajectòria, realitzat amb petits impulsos del sistema de propulsió del satèl·lit en lo que s'anomena una maniobra. Quan un satèl·lit es troba en una maniobra, deixa de seguir els models de caiguda lliure, per tant la maniobra s'ha de tenir en conte en l'estimació del filtre.
Tots els algoritmes i mètodes dissenyats han sigut testejats amb dades reals de diferents missions: SAC-C, CHAMP, JASON-1 i GRACE. S'han fet servir diversos tests cobrint diferents opcions de parametrització per tal d'avaluar el seu comportament.
Se define un satélite de órbita baja aquel que se encuentra en una altura de hasta 2000 km sobre la superficie terrestre. Debido al rápido decaimiento de los objetos cercanos a la superficie debido al fregamiento atmosférico se acepta que la altura típica para un LEO se sitúa entre 200 y 2000 km.
Este rango de alturas hace que los LEO sean utilizados para un amplio rango de aplicaciones como repetidores de comunicaciones, sensores remotos, determinación gravimétrica y magnetométrica, altimetría oceánica, determinación atmosférica y en operaciones de Search and Rescue (Búsqueda y rescate). Su posicionamiento preciso es de gran importancia para poder cumplir correctamente con sus objetivos. En este sentido, una gran cantidad de satélites LEO disponen de un receptor GPS, que permite realizar medidas GPS durante todo su recorrido alrededor de la Tierra. Estas medidas puede ser utilizadas para determinar la trayectoria del satélite. Esta operación se suele realizar en tierra, después que el satélite haya retransmitido todas las medidas que ha tomado. La capacidad de hacer este posicionamiento en tiempo real a bordo del satélite es una necesidad para algunas aplicaciones. El posicionamiento autónomo es muy diferente al que se puede realizar en tierra, ya que los procesadores de satélites tienen limitaciones en recursos computacionales, y por tanto los complejos modelos y cálculos realizados en un ordenador normal en tierra son excesivos para un ordenador espacial. Además, algunos de los modelos utilizados en la estimación de la trayectoria necesitan datos adicionales (como actividad solar, o parámetros de rotación de la Tierra) que no están disponibles en tiempo real, por lo que hay que realizar algunas aproximaciones para no necesitar ninguno de estos datos. Esta tesis estudiará la navegación autónoma mediante GPS en satélites LEO, tendencia que esta aumentando su importancia por las aplicaciones tanto científicas como tecnológicas que se pueden derivar. La tesis desarrollara nuevos algoritmos y métodos para obtener una posición precisa y continua para LEOs. Se han cubierto diferentes aspectos:
· Mitigación de multipath e interferencias. Las reflexiones de las señales GPS en la estructura del satélite crea una distorsión que afecta la distancia medida. La repetibilidad de estos efectos en relación con la orientación del satélite puede ser utilizado para mitigar su impacto en la solución de navegación. Se han desarrollado técnicas de mitigación de multipath e interferencias para receptores de una o dos frecuencias.
· Modelos dinámicos de fuerzas. La trayectoria de objetos orbitando la Tierra es muy predecible, lo cual puede ser usado en sinergia con GPS para conseguir posiciones más precisas que usando solo GPS. Esto se utiliza normalmente en estrategias en postproceso, pero tiene grandes necesidades computacionales, y requiere de parámetros no disponibles en tiempo real. La simplificación de estos modelos, y la supresión e esos parámetros es necesario para poder aplicar esta técnica de procesado en condiciones de tiempo real.
· Maniobras. Los cuerpos en órbita alrededor de la Tierra no siguen una trayectoria perfectamente predecible. Hay pequeñas perturbaciones que modifican su trayectoria a largo plazo. Además el fregamiento atmosférico frena poco a poco el satélite, reduciendo su altura. Esto hace que sea necesaria una corrección periódica de su trayectoria, realizado en pequeños impulsos por el sistema de propulsión del satélite en lo que se llama una maniobra. Cuando un satélite realiza una maniobra deja de comportarse según los modelos de caida libre, por tanto su maniobra se ha de tener en cuenta en la estimación del filtro. Todos los algoritmos y métodos diseñados han sido testeados con datos reales de diferentes misiones: SAC-C, CHAMP, JASON-1 y GRACE. Se han realizado un amplio abanico de tests cubriendo diferentes opciones de parametrización para evaluar su comportamiento.
Satellites in low Earth orbits (LEO) are generally defined to be up to an altitude of 2000 km above Earth's surface and given the rapid decay of objects on the lower altitude range due to atmospheric drag, it is commonly accepted that a typical LEO height lies between 200 and 2000 km. This altitude range makes LEO satellites useful for a wide range of applications such as communication transponders, remote sensing, gravimetric and magnetometric sounding, ocean altimetry, atmospheric retrieval and Search and Rescue alarm operations. Its accurate positioning is of great importance in the successful accomplishment of their objectives. In this sense, most LEO satellites have a GPS receiver, which allows to collect GPS measurements in its full revolution around the Earth. These measures can be used to precisely estimate the trajectory of the spacecraft. This operation is normally done on ground, after the satellite was able to downlink all the data it collected. The capacity to do this positioning in real-time onboard the satellite is a necessity for some of the applications, and would also allow a faster science product delivery.
This autonomous positioning is very different that the one that can be done on ground, as the satellite processor has large limitations in computational resources, so the complex models and calculus done in a normal computer on ground are completely unaffordable for the onboard processor. Besides, some of the models used in the trajectory estimation need some additional data (such as solar activity, or Earth rotation parameters) that are not available in real-time, so some approximations must be done to cope with these lack of data. This thesis will deepen into the study of autonomous GPS navigation of LEO satellites, a trend that is increasing its importance for their applications in both science and technological fields. It will develop new algorithms and methods in order to provide accurate and continuous positions for the satellites. Different aspects have been covered:
· Multipath and interference mitigation. Reflections of GPS signals in the spacecraft structure cause a distress that affects the measured distance. On the other hand, some spacecraft have more than one GPS antenna on its payload. This creates a cross-talk interference that also affects the measures. The repeatability of these effects in relation to the attitude of the spacecraft can be used to mitigate its impact into the final navigation solution. Multipath mitigation techniques have been developed for both single- and dual-frequency receivers.
· Dynamic force models. The high predictability of the trajectory of Earth orbiters is used in conjunction to GPS measurements to provide a more accurate solution than GPS standalone positions. This is a widely used technique in postprocessing strategies, but has high computational requirements and needs parameters not available in real-time. The simplifications of these models, along with the suppression of the parameters not available in an onboard environment is necessary to use these kind of positioning by a satellite processing in real-time conditions.
· Maneuver handling. Earth orbiters do not follow a fully predictable orbit, some low-order perturbations modifies its trajectory on the long term, and atmospheric drag slowly brakes the satellite, decreasing its altitude. This makes necessary a periodic correction of its trajectory.
This is done by short impulses produced by the satellite propulsion systems in what is called a maneuver. When a spacecraft is in a maneuver, it no longer follows the free-flight dynamic models, so this should be taken into account in the estimation filter. All the algorithms and methods have been tested with real data from different missions: SAC-C, CHAMP, JASON-1 and GRACE. Several test cases covering a wide range of days and parametrization options have been done in order to assess its performance.
Tao, Zui. "Autonomous road vehicles localization using satellites, lane markings and vision." Thesis, Compiègne, 2016. http://www.theses.fr/2016COMP2261/document.
Full textEstimating the pose (position and attitude) in real-time is a key function for road autonomous vehicles. This thesis aims at studying vehicle localization performance using low cost automotive sensors. Three kinds of sensors are considered : dead reckoning (DR) sensors that already exist in modern vehicles, mono-frequency GNSS (Global navigation satellite system) receivers with patch antennas and a frontlooking lane detection camera. Highly accurate maps enhanced with road features are also key components for autonomous vehicle navigation. In this work, a lane marking map with decimeter-level accuracy is considered. The localization problem is studied in a local East-North-Up (ENU) working frame. Indeed, the localization outputs are used in real-time as inputs to a path planner and a motion generator to make a valet vehicle able to drive autonomously at low speed with nobody on-board the car. The use of a lane detection camera makes possible to exploit lane marking information stored in the georeferenced map. A lane marking detection module detects the vehicle’s host lane and provides the lateral distance between the detected lane marking and the vehicle. The camera is also able to identify the type of the detected lane markings (e.g., solid or dashed). Since the camera gives relative measurements, the important step is to link the measures with the vehicle’s state. A refined camera observation model is proposed. It expresses the camera metric measurements as a function of the vehicle’s state vector and the parameters of the detected lane markings. However, the use of a camera alone has some limitations. For example, lane markings can be missing in some parts of the navigation area and the camera sometimes fails to detect the lane markings in particular at cross-roads. GNSS, which is mandatory for cold start initialization, can be used also continuously in the multi-sensor localization system as done often when GNSS compensates for the DR drift. GNSS positioning errors can’t be modeled as white noises in particular with low cost mono-frequency receivers working in a standalone way, due to the unknown delays when the satellites signals cross the atmosphere and real-time satellites orbits errors. GNSS can also be affected by strong biases which are mainly due to multipath effect. This thesis studies GNSS biases shaping models that are used in the localization solver by augmenting the state vector. An abrupt bias due to multipath is seen as an outlier that has to be rejected by the filter. Depending on the information flows between the GNSS receiver and the other components of the localization system, data-fusion architectures are commonly referred to as loosely coupled (GNSS fixes and velocities) and tightly coupled (raw pseudoranges and Dopplers for the satellites in view). This thesis investigates both approaches. In particular, a road-invariant approach is proposed to handle a refined modeling of the GNSS error in the loosely coupled approach since the camera can only improve the localization performance in the lateral direction of the road. Finally, this research discusses some map-matching issues for instance when the uncertainty domain of the vehicle state becomes large if the camera is blind. It is challenging in this case to distinguish between different lanes when the camera retrieves lane marking measurements.As many outdoor experiments have been carried out with equipped vehicles, every problem addressed in this thesis is evaluated with real data. The different studied approaches that perform the data fusion of DR, GNSS, camera and lane marking map are compared and several conclusions are drawn on the fusion architecture choice
Mignot, Shan. "Towards a demonstrator for autonomous object detection on board Gaia." Observatoire de Paris (1667-....), 2008. https://theses.hal.science/tel-00340279v2.
Full textESA's cornerstone mission Gaia aims at building a star catalogue limited only by their magnitudes. The expected billion objects must be detected on board in real-time before they can be observed and the scientific and technical requirements make this an engineering challenge. We have devised a prototype to assess achievable performances and assist in sizing the on-board electronics (PDHE TDA). It is based on a sequence of four tasks: calibrating the incoming data from the CCDs, estimating the sky background, identifying the objects and, finally, characterising them to command subsequent observations. Although inspired by previous similar studies (APM, Sextractor), this approach has been thoroughly revisited and finely adapted to Gaia. Following the recommendations of the PDHE TDA, a mixed implementation is proposed which deals with the important data flow and the hard real-time constraints in hardware (FPGA) and entrusts more complex or variable processing to software. The segmentation also corresponds to subdividing the previous operations in pixel-based and object-based domains. Our demonstrator shows that the scientific specifications are met in terms of completeness, of precision and of robustness to the variety of observing conditions while, technically speaking, our pipeline, optimised for area and power consumption, allows for identifying a target technology. Our model has not been retained for the industrial phases of Gaia but, beside it recognised usefulness in the project, represents R&D for the forthcoming generation of satellites
Porter, Robert D. "Development and control of the Naval Postgraduate School Planar Autonomous Docking Simulator (NPADS) /." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://library.nps.navy.mil/uhtbin/hyperion-image/02sep%5FPorter.pdf.
Full textThesis advisor(s): Michael G. Spencer, Brij N. Agrawal. Includes bibliographical references (p. 83). Also available online.
McConnell, Joshua B. (Joshua Bryan) 1974. "Technical and policy issues surrounding the use of autonomous maneuverable earth observing satellites." Thesis, Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/82781.
Full textIncludes bibliographical references (leaves 237-240).
by Joshua B. McConnell.
S.M.
Bayoudh, Mehdi. "Active Diagnosis of Hybrid Systems Guided by Diagnosability Properties - Application to Autonomous Satellites." Thesis, Toulouse, INPT, 2009. http://www.theses.fr/2009INPT069H.
Full textMotivated by the requirements of the space domain in terms of on-board diagnosis and autonomy, this thesis addresses the problems of diagnosis, diagnosability and active diagnosis of hybrid systems. Supported by a hybrid modeling framework, a passive approach for model-based diagnosis mixing discrete-event and continuous techniques is proposed. The same hybrid model is used to define the diagnosability property for hybrid systems and diagnosability criteria are derived. When the diagnosis provided by the passive diagnosis approach is ambiguous, active diagnosis is needed. This work provides a method for performing such active diagnosis. Starting with an ambiguous belief state, the method calls for diagnosability analysis results to determine a new system configuration in which fault candidates can be discriminated. Based on a new finite state machine called the diagnoser, the active diagnosis is formulated as a conditional planning problem and an AND-OR graph exploration algorithm is proposed to determine active diagnosis plans. Finally, the diagnosis approach is tested on the Attitude Control System (ACS) of a satellite simulator provided by Thales Alenia Space. The diagnosis module is successfully tested on several fault scenarios and the obtained results are reported
Mienie, Dewald. "Autonomous docking for a satellite pair using monocular vision." Thesis, Stellenbosch : University of Stellenbosch, 2009. http://hdl.handle.net/10019.1/2382.
Full textAutonomous rendezvouz and docking is seen as an enabling technology. It allows, among others, the construction of larger space platforms in-orbit and also provides a means for the in-orbit servicing of space vehicles. In this thesis a docking sequence is proposed and tested in both simulation and practice. This therefore also requires the design and construction of a test platform. A model hovercraft is used to emulate the chaser satellite in a 2-dimensional plane as it moves relatively frictionlessly. The hovercraft is also equipped with a single camera (monocular vision) that is used as the main sensor to estimate the target’s pose (relative position and orientation). An imitation of a target satellite was made and equipped with light markers that are used by the chaser’s camera sensor. The position of the target’s lights in the image is used to determine the target’s pose using a modified version ofMalan’s Extended Kalman Filter [20]. This information is then used during the docking sequence. This thesis successfully demonstrated the autonomous and reliable identification of the target’s lights in the image, and the autonomous docking of a satellite pair using monocular camera vision in both simulation and emulation.
Serdar, Saliha. "Design of an Autonomous Decision Support System for High-Level Planning in Nano Satellites Using Logic Programming." Thesis, Luleå tekniska universitet, Institutionen för system- och rymdteknik, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61239.
Full textAbedini, A., J. Moriarta, D. Biroscak, L. Losik, and R. F. Malina. "A Low-Cost, Autonomous, Ground Station Operations Concept and Network Design for EUVE and Other Earth-Orbiting Satellites." International Foundation for Telemetering, 1995. http://hdl.handle.net/10150/608538.
Full textThe Extreme Ultraviolet Explorer (EUVE) satellite was designed to operate with the Tracking and Data Relay Satellite System (TDRSS) and Deep Space Network (DSN). NASA, the Jet Propulsion Laboratory and the Center for EUV Astrophysics have been evaluating a commercially available ground station already used for NASA's Low Earth Orbit (LEO) weather satellites. This ground station will be used in a network of unattended, autonomous ground stations for telemetry reception, processing, and routing of data over a commercial, secure data line. Plans call for EUVE to be the initial network user. This network will be designed to support many TDRSS/DSN compatible missions. It will open an era of commercial, low-cost, autonomous ground station networks. The network will be capable of supporting current and future NASA scientific missions, and NASA's LEO and geostationary weather satellites. Additionally, it could support future, commercial communication satellites in low, and possibly medium, Earth orbit. The combination of an autonomous ground station and an autonomous telemetry monitoring system will allow reduction in personnel. The EUVE Science Operations Center has already reduced console work from three shifts to one by use of autonomous telemetry monitoring software.
Cristini, Frédéric. "Amélioration de la résilience de systèmes spatiaux soumis à des menaces : vers des réseaux de satellites autonomes." Thesis, Toulouse, ISAE, 2014. http://www.theses.fr/2014ESAE0025/document.
Full textAlthough Earth observation space systems are designed with strong safety requirements due to an hostile natural space environment, they remain vulnerable to an increasing range of emerging space threats such as antisatellite weapons or orbital debris. Instead of a physical protection of these monolithic and remote-controlled assets, we propose a design strategy based on the concept of resilience which is the ability of a system to maintain an acceptable level of performance in the presence of unforeseeable disturbance.Thanks to the latest space technology innovations, we devised new system architectures composed of networked constellations of heterogeneous and autonomous interacting microsatellites. We decided to model these architectures, called autonomous networked constellations (RCA in French), thanks to Petri nets, and more specifically their nets-within-nets variant. Using telecommunication and multiagent metrics, we assessed different RCA configurations through their operational performance and communicability, for nominal as wellas degraded modes. From the resilience point of view, we present quantitative results that point out the benefits of dense space networks and embedded autonomous reconfiguration modules
Browne, Daniel C. "Enabling collaborative behaviors among cubesats." Thesis, Georgia Institute of Technology, 2011. http://hdl.handle.net/1853/41223.
Full textAnderson, Mike, Peter Militch, and Hugh Pickens. "AN AUTONOMOUS SATELLITE TRACKING STATION." International Foundation for Telemetering, 1999. http://hdl.handle.net/10150/607307.
Full textIn 1998, AlliedSignal Technical Services (ATSC) installed three fully autonomous 13-meter satellite tracking systems for the Integrated Program Office of the National Oceanic and Atmospheric Administration (NOAA) at the Command and Data Acquisition Station near Fairbanks, Alaska. These systems track and command NOAA Polar Orbiting Weather Satellites and Defense Meteorological Satellites. Each tracking system operates for extended periods of time with little intervention other than periodic scheduling contacts. Schedule execution initiates equipment configuration, including establishing the RF communications link to the satellite. Station autonomy is achieved through use of a robust scheduler that permits remote users and the System Administrator to request pass activities for any of the supported missions. Spacecraft in the mission set are scheduled for normal operations according to the priority they have been assigned. Once the scheduler resolves conflicts, it builds a human-readable control script that executes all required support activities. Pass adds or deletes generate new schedule scripts and can be performed in seconds. The systems can be configured to support CCSDS and TDM telemetry processing, but the units installed at Fairbanks required only telemetry and command through-put capabilities. Received telemetry data is buffered on disk-storage for immediate, post-pass playback, and also on tape for long-term archiving purposes. The system can autonomously support up to 20 spacecraft with 5 different configuration setups each. L-Band, S-Band and X-Band frequencies are supported.
Sauer, Birgit M. (Birgit Maria) 1971. "Autonomous mission scheduling for satellite operations." Thesis, Massachusetts Institute of Technology, 1997. http://hdl.handle.net/1721.1/49978.
Full textKaiser, Julius A., and Fredrick W. Herold. "AUTONOMOUS GROUND STATION FOR SATELLITE COMMUNICATIONS." International Foundation for Telemetering, 1999. http://hdl.handle.net/10150/607306.
Full textEmployment of the retro-directive technique described in Reference 1 describes a totally Autonomous Ground Station providing hemispheric coverage and continuous tracking. This System establishes communications between the satellite and ground station without human intervention or moving parts. When a satellite is in view, the ground station beacon antenna, using CDMA, enables the desired satellite transmitter and directs its beam to the ground station. The ground station, using the satellite’s transmitted signal, directs it’s receive and transmit arrays to point the ground station beams to the satellite, establishing two-way communications. The process is automatic and provides continuous horizon to horizon tracking.
Araguz, López Carles. "In pursuit of autonomous distributed satellite systems." Doctoral thesis, Universitat Politècnica de Catalunya, 2019. http://hdl.handle.net/10803/668234.
Full textLa imatgeria per satèl·lit ha esdevingut un recurs essencial per assolir tasques ambientals, humanitàries o industrials. Per tal de satisfer els requeriments de les noves aplicacions i usuaris, els sistemes d’observació de la Terra (OT) estan explorant la idoneïtat dels Sistemes de Satèl·lit Distribuïts (SSD), on múltiples observatoris espacials mesuren el planeta simultàniament. Degut al les resolucions temporals i espacials requerides, els SSD sovint es conceben com sistemes de gran escala que operen en xarxa. Aquestes noves arquitectures promouen les capacitats emergents dels sistemes distribuïts i, tot i que són possibles gràcies a l’acceptació de les plataformes de satèl·lits petits, encara presenten molts reptes en quant al disseny i operacions. Dos d’ells són els pilars principals d’aquesta tesi, en concret, la concepció d’eines de suport a la presa de decisions pel disseny de SSD, i la definició d’operacions autònomes basades en gestió descentralitzada a bord dels satèl·lits. La primera part d’aquesta dissertació es centra en el disseny arquitectural de SSD heterogenis i en xarxa, imbricant tecnologies de petits satèl·lits amb actius tradicionals. Es presenta un entorn d’optimització orientat al disseny basat en metodologies d’exploració i comparació de solucions. Els objectius d’aquest entorn són: la selecció el disseny de constel·lació més òptim; i facilitar la identificació de tendències de disseny, regions d’incompatibilitat, i tensions entre atributs arquitecturals. Sovint en els SSD d’OT, els requeriments del sistema i l’expressió de prioritats no només s’articulen en quant als atributs funcionals o les restriccions monetàries, sinó també a través de les característiques qualitatives com la flexibilitat, l’evolucionabilitat, la robustesa, o la resiliència, entre d’altres. En línia amb això, l’entorn d’optimització defineix una única figura de mèrit que agrega rendiment, cost i atributs qualitatius. Així l’equip de disseny pot influir en les solucions del procés d’optimització tant en els aspectes quantitatius, com en les característiques dalt nivell. L’aplicació d’aquest entorn d’optimització s’il·lustra en dos casos d’ús actuals identificats en context del projecte europeu ONION: un sistema que mesura paràmetres de l’oceà i gel als pols per millorar la predicció meteorològica i les operacions marines; i un sistema que obté mesures agronòmiques vitals per la gestió global de l’aigua, l’estimació d’estat dels cultius, i la gestió de sequeres. L’anàlisi de propietats arquitecturals ha permès copsar de manera exhaustiva les característiques funcionals i operacionals d’aquests sistemes. Amb això, la tesi ha seguit aprofundint en el disseny de SSD centrant-se, particularment, en un tret funcional: l’autonomia. Minimitzar la intervenció de l’operador humà és comú en altres sistemes espacials i podria ser especialment crític pels SSD de gran escala, d’estructura dinàmica i heterogenis. En els SSD s’espera que l’autonomia solucioni la possible incapacitat d’operar sistemes de gran escala de forma centralitzada, que millori el retorn científic i que n’apuntali les seves propietats emergents (e.g. tolerància a errors, adaptabilitat a canvis estructural i de necessitats d’usuari, capacitat de resposta). Es proposa un sistema d’operacions autònomes que atorga la capacitat de gestionar els sistemes de forma descentralitzada, a través del raonament local, l’assignació individual de recursos, i les interaccions satèl·lit-a-satèl·lit. Al contrari que treballs anteriors, la presa de decisions autònoma s’avalua per constel·lacions que tenen com a objectius de missió la minimització del temps de revisita global.
Eckert, M., C. Smith, F. Kronberg, F. Girouard, A. Hopkins, L. Wong, P. Ringrose, B. Stroozas, and R. F. Malina. "EUVE Telemetry Processing and Filtering for Autonomous Satellite Instrument Monitoring." International Foundation for Telemetering, 1996. http://hdl.handle.net/10150/611477.
Full textA strategy for addressing the complexity of problem identification and notification by autonomous telemetry monitoring software is discussed. The Extreme Ultraviolet Explorer (EUVE) satellite's science operations center (ESOC) is completing a transition to autonomous operations. Originally staffed by two people, twenty-four hours every day, the ESOC is nearing the end of a phased transition to unstaffed monitoring of the science payload health. To develop criteria for the implementation of autonomous operations we first identified and analyzed potential risk areas. These risk areas were then considered in light of a fully staffed operations model, and in several reduced staffing models. By understanding the accepted risk in the nominal, fully staffed model, we could define what criteria to use in comparing the effectiveness of reduced staff models. The state of the scientific instrument package for EUVE is evaluated by a rule-based telemetry processing software package. In the fully automated implementation, anomalous states are characterized in three tiers: critical to immediate instrument health and safety, non-critical to immediate instrument health and safety, and affecting science data only. Each state requires specific action on the part of the engineering staff, and the response time is determined by the tier. The strategy for implementing this prioritized, autonomous instrument monitoring and paging system is presented. We have experienced a variety of problems in our implementation of this strategy, many of which we have overcome. Problems addressed include: dealing with data dropouts, determining if instrument knowledge is current, reducing the number of times personnel are paged for a single problem, prohibiting redundant notification of known problems, delaying notification of problems for instrument states that do not jeopardize the immediate health of the instrument, assuring a response to problems in a timely manner by engineering staff, and communicating problems and response status among responsible personnel.
Tripp, Howard J. A. "Stigmergy for autonomous distributed coordination of satellite clusters." Thesis, University of Surrey, 2009. http://epubs.surrey.ac.uk/771933/.
Full textTurner, Tim. "Autonomous Control and Data Acquisition for Advanced Satellite Systems." International Foundation for Telemetering, 1985. http://hdl.handle.net/10150/615595.
Full textAutonomous operation is rapidly becoming a requirement for most new spacecraft systems. An autonomous spacecraft greatly simplifies the ground station processing and monitoring requirements, freeing ground station capabilities for other important tasks. The T2C2 (Telemetry, Timing, Command and Control) System has been conceived and architected to facilitate spacecraft autonomy. The T2C2 architecture is ideally suited for onboard closed-loop control, redundancy management, housekeeping and other autonomous functions. This paper provides an overview of the T2C2 architecture and its applications in the design and implementation of an autonomous spacecraft.
Raveneau, Patrice. "Satellites d'observation et réseaux de capteurs autonomes au service de l'environnement." Phd thesis, Toulouse, INPT, 2014. http://oatao.univ-toulouse.fr/11965/1/raveneau.pdf.
Full textRivera, Pablo Abraham. "Development of an autonomous rover for the Nevada student satellite program." abstract and full text PDF (free order & download UNR users only), 2007. http://0-gateway.proquest.com.innopac.library.unr.edu/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqdiss&rft_dat=xri:pqdiss:1446452.
Full textDiaz, Jorge Enrique Espíndola. "An autonomous and dynamical approach to small satellite ground stations networks." Instituto Nacional de Pesquisas Espaciais (INPE), 2017. http://urlib.net/sid.inpe.br/mtc-m21b/2017/07.04.19.59.
Full textOs custos nas operações de satélites geralmente não são desprezíveis, especialmente para missões de longa duração. Uma alternativa para baratear custos é aumentar o nível de automação em procedimentos quando for possível. Este trabalho de tese propõe uma abordagem dinâmica e autônoma para operações espaciais em redes de estações terrenas para pequenos satélites que visa minimizar seus custos operacionais. A solução proposta denomina-se ADSGS (Autonomous and Dynamic System Ground Station em Inglês) e é um middleware com componentes de hardware e software para atuação em um ambiente distribuído em uma rede de estações terrenas. Neste trabalho foi adotada a rede SATNet que carece de um componente de alocação com as características de dinamismo e autonomia. No ADSGS isto é oferecido mediante o uso da inteligência artificial em um sistema especialista baseado em regras. Na proposta, um agente de rede da ADSGS atua autônoma e dinamicamente na rede SATNet onde se gerenciam componentes das estações associadas. O agente ADSGS utiliza uma versão estendida do Algoritmo Húngaro para otimização combinatória de problemas de alocação e responder a eventos como interrupção de serviços. O componente de hardware proposto utiliza elementos de hardware COTS e tecnologia SDR (Software Defined Radio) ao passo que o componente de software utiliza pacotes como Orbitron, ProEst, o sistema especialista SINTA, entre outros. A modelagem UML é oferecida para documentar o componente de software. Um estudo de caso é feito para ilustrar as principais funcionalidades do ADSGS consistindo de uma pequena simulação em MATLAB com STK (Systems Tool Kit) e dois cenários de designação (1-to-m e n-to-m) de estações na rede SATNet a satélites pelo agente ADSGS.
Lange, Connor. "A GENERIC DECISION MAKING FRAMEWORK FOR AUTONOMOUS SYSTEMS." DigitalCommons@CalPoly, 2013. https://digitalcommons.calpoly.edu/theses/992.
Full textStroozas, B. A., D. Biroscak, M. Eckert, F. Girouard, A. Hopkins, G. C. Kaplan, F. Kronberg, et al. "The NASA EUVE Satellite in Transition: From Staffed to Autonomous Science Payload Operations." International Foundation for Telemetering, 1996. http://hdl.handle.net/10150/611421.
Full textThe science payload for NASA's Extreme Ultraviolet Explorer (EUVE) satellite is controlled from the EUVE Science Operations Center (ESOC) at the Center for EUV Astrophysics (CEA), University of California, Berkeley (UCB). The ESOC is in the process of a transition from a single staffed shift to an autonomous, zero-shift, "lights out" science payload operations scenario (a.k.a., 1:0). The purpose of the 1:0 transition is to automate all of the remaining routine, daily, controller telemetry monitoring and associated "shift" work. Building on the ESOC's recent success moving from three-shift to one-shift operations (completed in Feb 1995), the 1:0 transition will further reduce payload operations costs and will be a "proof of concept" for future missions; it is also in line with NASA's goals of "cheaper, faster, better" operations and with its desire to out-source missions like EUVE to academe and industry. This paper describes the 1:0 transition for the EUVE science payload: the purpose, goals, and benefits; the relevant science payload instrument health and safety considerations; the requirements for, and implementation of, the multi-phased approach; a cost/benefit analysis; and the various lessons learned along the way.
Schultz, Christopher R. "An Autonomous Underwater Vehicle for Validating Internal Actuator Control Strategies." Thesis, Virginia Tech, 2006. http://hdl.handle.net/10919/33190.
Full text
The Internally Actuated, Modular Bodied, Untethered Submersible (IAMBUS) can be used to validate non-linear control strategies using internal actuators. Vehicle attitude control is provided by three orthogonally mounted reaction wheels. The housing is a spherical glass pressure vessel, which contains all of the components, such as actuators, ballast system, power supply, on-board computer and inertial sensor. Since the housing is spherically symmetric, the hydrodynamics of IAMBUS are uncoupled (e.g. a roll maneuver does not impact pitch or yaw). This hull shape enables IAMBUS to be used as a spacecraft attitude dynamics and control simulator with full rotational freedom.
Master of Science
Grubinger, Michael, and Felix Strohmeier. "AUTONOMOUS ACQUISITION OF ENVIRONMENTAL DATA IN A GLOBAL NETWORK ENVIRONMENT." International Foundation for Telemetering, 2001. http://hdl.handle.net/10150/607597.
Full textThis paper presents the results of a feasibility study undertaken by the University of Salzburg (Austria), investigating the autonomous acquisition of environmental data in a global network. A suggested application which is used as the basis of this paper is a volcano monitoring system which would be able to track the activity of a volcano and act as a disaster warning system. The background Volcano observation data required for such a system is covered, before discussing the concepts for sensor data acquisition, storage and processing. A final analysis is then presented of the opportunities for the transmission by packet radio (both terrestrial and satellite).
Ortolano, Nicholas G. "Autonomous Trajectory Planning for Satellite RPO and Safety of Flight Using Convex Optimization." DigitalCommons@USU, 2018. https://digitalcommons.usu.edu/etd/7291.
Full textHultberg, Johanna. "Dehazing of Satellite Images." Thesis, Linköpings universitet, Datorseende, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-148044.
Full textSteindorf, Lukas. "Constrained Low-Thrust Satellite Formation-Flying Using Relative Orbit Elements : Autonomous Guidance and Control for the NetSat Satellite Formation-Flying Mission." Thesis, Luleå tekniska universitet, Institutionen för system- och rymdteknik, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61599.
Full textSimard, Bilodeau Vincent. "Lois de commande prédictives autonomes pour vol en formation de satellites terrestres." Mémoire, Université de Sherbrooke, 2008. http://savoirs.usherbrooke.ca/handle/11143/1469.
Full textGasslander, Maja. "Segmentation of Clouds in Satellite Images." Thesis, Linköpings universitet, Datorseende, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-128802.
Full textBénazéra, Emmanuel. "Diagnostic et reconfiguration basés sur des modèles hybrides concurrents : application aux satellites autonomes." Toulouse 3, 2003. http://www.theses.fr/2003TOU30105.
Full textWojtulewicz, Karol, and Viktor Agbrink. "Evaluating DCNN architecturesfor multinomial area classicationusing satellite data." Thesis, Linköpings universitet, Artificiell intelligens och integrerade datorsystem, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-168805.
Full textNolet, Simon 1975. "Development of a guidance, navigation and control architecture and validation process enabling autonomous docking to a tumbling satellite." Thesis, Massachusetts Institute of Technology, 2007. http://hdl.handle.net/1721.1/39697.
Full textIncludes bibliographical references (p. 307-324).
The capability to routinely perform autonomous docking is a key enabling technology for future space exploration, as well as assembly and servicing missions for spacecraft and commercial satellites. Particularly, in more challenging situations where the target spacecraft or satellite is tumbling, algorithms and strategies must be implemented to ensure the safety of both docking entities in the event of anomalies. However, difficulties encountered in past docking missions conducted with expensive satellites on orbit have indicated a lack of maturity in the technologies required for such operations. Therefore, more experimentation must be performed to improve the current autonomous docking capabilities. The main objectives of the research presented in this thesis are to develop a guidance, navigation and control (GN&C) architecture that enables the safe and fuel-efficient docking with a free tumbling target in the presence of obstacles and anomalies, and to develop the software tools and verification processes necessary in order to successfully demonstrate the GN&C architecture in a relevant environment. The GN&C architecture was developed by integrating a spectrum of GN&C algorithms including estimation, control, path planning, and failure detection, isolation and recovery algorithms.
(cont.) The algorithms were implemented in GN&C software modules for real-time experimentation using the Synchronized Position Hold Engage and Reorient Experimental Satellite (SPHERES) facility that was created by the MIT Space Systems Laboratory. Operated inside the International Space Station (ISS), SPHERES allow the incremental maturation of formation flight and autonomous docking algorithms in a risk-tolerant, microgravity environment. Multiple autonomous docking operations have been performed in the ISS to validate the GN&C architecture. These experiments led to the first autonomous docking with a tumbling target ever achieved in microgravity. Furthermore, the author also demonstrated successful docking in spite of the presence of measurement errors that were detected and rejected by an online fault detection algorithm. The results of these experiments will be discussed in this thesis. Finally, based on experiments in a laboratory environment, the author establishes two processes for the verification of GN&C software prior to on-orbit testing on the SPHERES testbed.
by Simon Nolet.
Sc.D.
Norris, Natasha Louise. "Implementation of Multi-Constellation Baseline Fault Detection and Exclusion Algorithm Utilizing GPS and GLONASS Signals." Ohio University / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1535028817622931.
Full textTorén, Rickard. "Comparing CNN methods for detection and tracking of ships in satellite images." Thesis, Linköpings universitet, Institutionen för datavetenskap, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-167163.
Full textKronberg, F., P. Ringrose, L. Losik, D. Biroscak, and R. F. Malina. "RE-ENGINEERING THE EUVE PAYLOAD OPERATIONS INFORMATION FLOW PROCESS TO SUPPORT AUTONOMOUS MONITORING OF PAYLOAD TELEMETRY." International Foundation for Telemetering, 1995. http://hdl.handle.net/10150/608529.
Full textThe UC Berkeley Extreme Ultraviolet Explorer (EUVE) Science Operations Center (ESOC) is developing and implementing knowledge-based software to automate the monitoring of satellite payload telemetry. Formerly, EUVE science payload data were received, archived, interpreted, and responded to during round-the-clock monitoring by human operators. Now, knowledge-based software will support, augment, and supplement human intervention. In response to and as a result of this re-engineering project, the creation, storage, revision, and communication of information (the information flow process) within the ESOC has been redesigned. We review the information flow process within the ESOC before, during, and after the re-engineering of telemetry monitoring. We identify six fundamental challenges we face in modifying the information flow process. (These modifications are necessary because of the shift from continuous human monitoring to a knowledge-based autonomous monitoring system with intermittent human response.) We describe the innovations we have implemented in the ESOC information systems, including innovations in each part of the information flow process for short-term or dynamic information (which changes or updates within a week) as well as for long-term or static information (which is valid for more than a week). We discuss our phased approach to these innovations, in which modifications were made in small increments and the lessons learned at each step were incorporated into subsequent modifications. We analyze some mistakes and present lessons learned from our experience.
Loizou, John. "An assessment of the autonomous integrity monitoring performance of a combined GPS/Galileo Satellite Navigation System, and its impact on the case for the development of Galileo." Thesis, Cranfield University, 2004. http://hdl.handle.net/1826/1604.
Full textCasadei, Alessandro. "An optical navigation filter simulator for a CubeSat mission to Didymos binary asteroid system." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2019. http://amslaurea.unibo.it/17998/.
Full textLi, Franck. "Lane-level vehicle localization with integrity monitoring for data aggregation." Thesis, Compiègne, 2018. http://www.theses.fr/2018COMP2458/document.
Full textThe information stored in digital road maps has become very important for intelligent vehicles. As intelligent vehicles address more complex environments, the accuracy requirements for this information have increased. Regarded as a geographic database, digital road maps contain contextual information about the road network, crucial for a good understanding of the environment. When combined with data acquired from on-board sensors, a better representation of the environment can be made, improving the vehicle’s situation understanding. Sensors performance can vary drastically depending on the location of the vehicle, mainly due to environmental factors. Comparatively, a map can provide prior information more reliably but to do so, it depends on another essential component: a localization system. Global Navigation Satellite Systems (GNSS) are commonly used in automotive to provide an absolute positioning of the vehicle, but its accuracy is not perfect: GNSS are prone to errors, also depending greatly on the environment (e.g., multipaths). Perception and localization systems are two important components of an intelligent vehicle whose performances vary in function of the vehicle location. This research focuses on their common denominator, the digital road map, and its use as a tool to assess their performance. The idea developed during this thesis is to use the map as a learning canvas, to store georeferenced information about the performance of the sensors during repetitive travels. This requires a robust localization with respect to the map to be available, through a process of map-matching. The main problematic is the discrepancy between the accuracy of the map and of the GNSS, creating ambiguous situations. This thesis develops a map-matching algorithm designed to cope with these ambiguities by providing multiple hypotheses when necessary. The objective is to ensure the integrity of the result by returning a hypothesis set containing the correct matching with high probability. The method relies on proprioceptive sensors via a dead-reckoning approach aided by the map. A coherence checking procedure using GNSS redundant information is then applied to isolate a single map-matching result that can be used to write learning data with confidence in the map. The possibility to handle the digital map in read/write operation has been assessed and the whole writing procedure has been tested on data recorded by test vehicles on open roads
"Improvements in autonomous GPS navigation of Low Earth Orbit satellites." Universitat Politècnica de Catalunya, 2008. http://www.tesisenxarxa.net/TDX-0312109-123420/.
Full textIbrahim, Najmus. "Attitude and Orbit Control of Small Satellites for Autonomous Terrestrial Target Tracking." Thesis, 2013. http://hdl.handle.net/1807/42965.
Full text