Bibliografie tematiche / Inertial navigation systems

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Letteratura scientifica selezionata sul tema "Inertial navigation systems"

Autore: Grafiati
Pubblicato: 4 giugno 2021
Ultima modifica: 30 luglio 2024

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Articoli di riviste sul tema "Inertial navigation systems"

1

Kortunov, V. I., I. Yu Dybska, G. A. Proskura, and T. Trachsel. "Accuracy Analysis of Strapdown Inertial Navigation Systems." Kosmìčna nauka ì tehnologìâ 13, no. 4 (July 30, 2007): 40–48. http://dx.doi.org/10.15407/knit2007.04.040.

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Turygin, Yuri, Pavol Božek, Yuri Nikitin, Ella Sosnovich, and Andrey Abramov. "Enhancing the reliability of mobile robots control process via reverse validation." International Journal of Advanced Robotic Systems 13, no. 6 (December 1, 2016): 172988141668052. http://dx.doi.org/10.1177/1729881416680521.

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Abstract (sommario):
The article deals with integrating the inertial navigation unit implemented into the system of controlling the robot. It analyses the dynamic properties of the sensors of the inertial unit, for example, gyroscopes and accelerometers. The implementation of the original system of controlling the mobile robot on the basis of autonomous navigation systems is a dominant part of the article. The integration of navigational information represents the actual issue of reaching higher accuracy of required navigational parameters using more or less accurate navigation systems. The inertial navigation is
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Szelmanowski, Andrzej, Mirosław Nowakowski, Zbigniew Jakielaszek, and Piotr Rogala. "Computer-based method for the technical condition evaluation of the Cardan inertial navigation system for the highly maneuverable aircraft." AUTOBUSY – Technika, Eksploatacja, Systemy Transportowe 20, no. 1-2 (February 28, 2019): 344–51. http://dx.doi.org/10.24136/atest.2019.064.

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Paper presents the original computer-based method of the technical condition evaluation of the analog inertial navigation systems on the basis of the calculated inertial speed course analysis. There are presented the mathematical relationships describing the influence of the angular velocity and linear accelerations sensors errors (used in inertial navigation systems on board the military aircraft) with the relation to the discrepancies of the calculated pilot-navigational parameters (such as inertial speed components and navigational position coordinates). On the example of the Cardan navigat
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He, Hongyang, Feng Zha, Feng Li, and Qiushuo Wei. "A Combination Scheme of Pure Strapdown and Dual-Axis Rotation Inertial Navigation Systems." Sensors 23, no. 6 (March 14, 2023): 3091. http://dx.doi.org/10.3390/s23063091.

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Compared with the strapdown inertial navigation system (SINS), the rotation strapdown inertial navigation system (RSINS) can effectively improve the accuracy of navigation information, but rotational modulation also leads to an increase in the oscillation frequency of attitude errors. In this paper, a dual-inertial navigation scheme that combines the strapdown inertial navigation system and the dual-axis rotation inertial navigation system is proposed, which can effectively improve the attitude error accuracy in the horizontal direction by using the high-position information of the rotation in
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Novikov, P. V., A. A. Sheypak, V. N. Gerdi, V. V. Novikov, and V. N. Enin. "Algorithm for navigation of ground-based transport-technological facilities on the basis of integrated inertial-satellite navigation and odometer data." Izvestiya MGTU MAMI 11, no. 2 (June 15, 2017): 31–39. http://dx.doi.org/10.17816/2074-0530-66895.

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The dynamic development of navigation technologies has led to the emergence of practical applications for the solution of the problem of navigation of ground transport and technological facilities (GTTF). The most promising way of solving the navigation problem of GTTF is the creation of integrated inertial-satellite navigation systems. For a long period of time, the widespread use of navigation systems for transport applications was constrained by their high cost. The appearance of low-cost microelectromechanical (MEMS) inertial sensors on the market of navigation equipment provided the techn
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Kovalenko, A. M., and A. A. Shejnikov. "Model of the inertial and optical navigation system of the unmanned aerial vehicle." «System analysis and applied information science», no. 2 (August 18, 2020): 17–25. http://dx.doi.org/10.21122/2309-4923-2020-2-17-25.

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In article approaches to creation of the complex inertial and optical navigation system of the short-range tactical unmanned aerial vehicle are considered. Algorithms constant and periodic (in intermediate points of a route) are offered correction of the platformless onboard inertial navigation system. At integration of information on parameters of the movement of the unmanned aerial vehicle (received from the considered systems) the invariant loosely coupled scheme of data processing on the basis of the expanded filter of Kallman was used that allowed to lower significantly a systematic compo
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Ushaq, Muhammad, and Jian Cheng Fang. "An Improved and Efficient Algorithm for SINS/GPS/Doppler Integrated Navigation Systems." Applied Mechanics and Materials 245 (December 2012): 323–29. http://dx.doi.org/10.4028/www.scientific.net/amm.245.323.

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Inertial navigation systems exhibit position errors that tend to grow with time in an unbounded mode. This degradation is due, in part, to errors in the initialization of the inertial measurement unit and inertial sensor imperfections such as accelerometer biases and gyroscope drifts. Mitigation to this growth and bounding the errors is to update the inertial navigation system periodically with external position (and/or velocity, attitude) fixes. The synergistic effect is obtained through external measurements updating the inertial navigation system using Kalman filter algorithm. It is a natur
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E, Topolskov, Beljaevskiy L. L, and Serdjuke A. "IMPROVEMENT OF NAVIGATION SYSTEMS OF VEHICLES BY MEANS OF INERTIAL SENSORS AND INFORMATION PROCESSING USING PROBABILITY-GEOMETRIC METHODS." National Transport University Bulletin 1, no. 46 (2020): 353–64. http://dx.doi.org/10.33744/2308-6645-2020-1-46-353-364.

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Providing high accuracy of the coordinates and trajectories of objects by measurements conducted in navigation systems and complexes is an urgent task, which improves safety and efficiency of different modes of transport. However difficult environmental conditions, where vehicles are commonly used, stipulate influence of different factors on performance of onboard satellite navigation receivers, which are used as basic navigation devices for ground vehicle nowadays. Setting on cars used for common purposes additional navigation devices, which provide better performance, in most cases is econom
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Vaispacher, Tomáš, Róbert Bréda, and František Adamčík. "Error Analysis of Inertial Navigation Systems Using Test Algorithms." Naše more 62, SI (October 2015): 204–8. http://dx.doi.org/10.17818/nm/2015/si21.

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Bodhare, Hemant Gautam, and Asst Prof Gauri Ansurkar. "LEO based Satellite Navigation and Anti-Theft Tracking System for Automobiles." International Journal for Research in Applied Science and Engineering Technology 10, no. 4 (April 30, 2022): 557–63. http://dx.doi.org/10.22214/ijraset.2022.41316.

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Abstract: GPS and Inertial Navigation Systems (INS) are used today in automobile navigation and tracking systems to locate themselves in Four Dimensions (latitude, longitude, altitude, time). However, GNSS or GPS still has its own bottleneck, such as the long initialization period of Precise Point Positioning (PPP) without dense reference network. For navigation, a number of selected LEO satellites can be equipped with a transmitter to transmit similar navigation signals to land users, so they can act like GNSS satellites but with much faster geometric change to enhance GNSS capability, which
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Tesi sul tema "Inertial navigation systems"

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Zhao, Yong 1980. "Discrete-time observers for inertial navigation systems." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/17956.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2004.<br>Includes bibliographical references (p. 65-66).<br>In this thesis, we derive an exact deterministic nonlinear observer to compute the continuous-time states of inertial navigation system based on partial discrete measurements, the so-called strapdown problem. Nonlinear contraction theory is used as the main analysis tool. The hierarchical structure of the system physics is sytematically exploited and the use of nonlinear measurements, such as distances to time-varying reference points, is discussed.
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Mohamadabadi, Kaveh. "Anisotropic Magnetoresistance Magnetometer for inertial navigation systems." Phd thesis, Ecole Polytechnique X, 2013. http://tel.archives-ouvertes.fr/tel-00946970.

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This work addresses the relevant errors of the anisotropic magnetoresistance sensor for inertial navigation systems. The manuscript provides resulting guidelines and solution for using the AMR sensors in a robust and appropriate way relative to the applications. New methods also are proposed to improve the performance and, reduce the power requirements and cost design of the magnetometer. The new compensation method is proposed by developing an optimization algorithm. The necessity of the sensor calibration is shown and the source of the errors and compensating model are investigated. Two nove
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Ruiz, Mario. "Optimization of a strapdown inertial navigation system." To access this resource online via ProQuest Dissertations and Theses @ UTEP, 2009. http://0-proquest.umi.com.lib.utep.edu/login?COPT=REJTPTU0YmImSU5UPTAmVkVSPTI=&clientId=2515.

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Hewitson, Steve Surveying &amp Spatial Information Systems Faculty of Engineering UNSW. "Quality control for integrated GNSS and inertial navigation systems." Awarded by:University of New South Wales. Surveying and Spatial Information Systems, 2006. http://handle.unsw.edu.au/1959.4/25534.

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The availability of GPS signals is a major limitation for many existing and potential applications. Fortunately, with the development of Galileo by the European Commission (EC) and European Space Agency (ESA) and new funding for the restoration of the Russian GLONASS announced by the Russian Federation the future for satellite based positioning and navigation applications is extremely promising. This research primarily investigates the benefits of GNSS interoperability and GNSS/INS integration to Receiver Autonomous Integrity Monitoring (RAIM) from a geometrical perspective. In addition to the
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Wall, John H. "A study of the effects of stochastic inertial sensor errors in dead-reckoning navigation." Auburn, Ala., 2007. http://repo.lib.auburn.edu/07M%20Theses/WALL_JOHN_59.pdf.

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Skog, Isaac. "Low-Cost Navigation Systems : A Study of Four Problems." Doctoral thesis, KTH, Signalbehandling, 2009. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-11736.

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Abstract (sommario):
Today the area of high-cost and high-performance navigation for vehicles is a well-developed field. The challenge now is to develop high-performance navigation systems using low-cost sensortechnology. This development involves problems spanning from signal processing of the dirty measurements produced by low-costsensors via fusion and synchronization of information produced by a large set of diverse sensors, to reducing the size and energyconsumption of the systems. This thesis examines and proposessolutions to four of these problems. The first problem examined is the time synchronizing of the
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Walchko, Kevin J. "Low cost inertial navigation learning to integrate noise and find your way /." [Gainesville, Fla.] : University of Florida, 2002. http://purl.fcla.edu/fcla/etd/UFE1001193.

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Li, Wei. "On the study of mixed signal interface circuit for inertial navigation system." Thesis, University of Macau, 2017. http://umaclib3.umac.mo/record=b3691765.

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Soloviev, Andrey. "Investigation into performance enhancement of integrated global positioning/inertial navigation systems by frequency domain implementation of inertial computational procedures." Ohio : Ohio University, 2002. http://www.ohiolink.edu/etd/view.cgi?ohiou1178652218.

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Sukkarieh, Salah. "Low Cost, High Integrity, Aided Inertial Navigation Systems for Autonomous Land Vehicles." Thesis, The University of Sydney, 2000. http://hdl.handle.net/2123/18358.

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This thesis describes the theoretical and practical development of a low cost, high integrity, aided inertial navigation system for use in autonomous land vehicle applications. The demand for fail safe navigation systems which can be used on large autonomous land vehicles such as those found in container terminals, agriculture, construction and in mines, has driven research and technology into the development of high integrity navigation suites. Integrity, in this thesis, is defined as the ability of a navigation system to provide reliable navigation information while also monitoring the healt
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Libri sul tema "Inertial navigation systems"

1

Britting, Kenneth R. Inertial navigation systems analysis. Boston: Artech House, 2010.

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P, Andrews Angus, Bartone Chris, and ebrary Inc, eds. Global navigation satellite systems, inertial navigation, and integration. 3rd ed. Hoboken: John Wiley & Sons, 2013.

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Siouris, George M. Aerospace avionics systems: A modern synthesis. San Diego: Academic Press, 1993.

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Weill, Lawrence R. (Lawrence Randolph), 1938-, Andrews Angus P, and Wiley online library, eds. Global positioning systems, inertial navigation, and integration. 2nd ed. Hoboken, N.J: Wiley-Interscience, 2007.

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1938-, Weill Lawrence Randolph, and Andrews Angus P, eds. Global positioning systems, inertial navigation, and integration. New York: John Wiley, 2001.

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L, Weston J., Institution of Electrical Engineers, and American Institute of Aeronautics and Astronautics., eds. Strapdown inertial navigation technology. 2nd ed. Stevenage: Institution of Electrical Engineers, 2004.

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L, Weston J., and Institution of Electrical Engineers, eds. Strapdown inertial navigation technology. London, UK: Peter Peregrinis Ltd. on behalf of the Institution of Electrical Engineers, 1997.

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Groves, Paul D. Principles of GNSS, inertial, and multisensor integrated navigation systems. Boston: Artech House, 2008.

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Khlebnikov, G. A. Nachalʹnai͡a︡ vystavka inert͡s︡ialʹnykh navigat͡s︡ionnykh sistem. Moskva: Voen. akademii͡a︡ im. F.Ė. Dzerzhinskogo, 1994.

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Shen, Chong. Intelligent Information Processing for Inertial-Based Navigation Systems. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-33-4516-4.

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Capitoli di libri sul tema "Inertial navigation systems"

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Zanetti, Renato, and Christopher D’Souza. "Inertial Navigation." In Encyclopedia of Systems and Control, 1–7. London: Springer London, 2020. http://dx.doi.org/10.1007/978-1-4471-5102-9_100036-1.

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Zanetti, Renato, and Christopher D’Souza. "Inertial Navigation." In Encyclopedia of Systems and Control, 993–99. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-44184-5_100036.

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Braasch, Michael S. "Inertial Navigation Systems." In Aerospace Navigation Systems, 1–25. Chichester, UK: John Wiley & Sons, Ltd, 2016. http://dx.doi.org/10.1002/9781119163060.ch1.

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Tooley, Mike, and David Wyatt. "Inertial navigation systems." In Aircraft Communications and Navigation Systems, 219–34. 3rd ed. London: Routledge, 2024. http://dx.doi.org/10.1201/9781003411932-15.

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Jekeli, Christopher. "Inertial Navigation Systems: Geodesy." In Encyclopedia of Geodesy, 1–8. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-02370-0_10-1.

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Bruder, Stephen, and Aly El-Osery. "Low-Cost Inertial Navigation." In Studies in Systems, Decision and Control, 231–59. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-14636-2_12.

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Lemmens, Mathias. "Global Navigation Satellite Systems and Inertial Navigation." In Geo-information, 55–83. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-1667-4_4.

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Gupta, Suresh Chandra. "Inertial Sensors and Navigation Systems." In The Mind of an Engineer, 427–32. Singapore: Springer Singapore, 2015. http://dx.doi.org/10.1007/978-981-10-0119-2_55.

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de Babo Martins, Francisco, Luis F. Teixeira, and Rui Nóbrega. "Visual-Inertial Based Autonomous Navigation." In Advances in Intelligent Systems and Computing, 561–72. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-27149-1_43.

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Aksonenko, P. M., V. V. Avrutov, Yu F. Lazarev, P. Henaff, and L. Ciarletta. "Expanded Algorithm for Inertial Navigation." In Advances in Intelligent Systems and Computing, 789–800. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-030-01177-2_58.

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Atti di convegni sul tema "Inertial navigation systems"

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Toda, Atsumi, and Yoshikazu Koike. "Simulation Design of Thermopile and Magnetometer Aided INS/GPS Navigation System for UAV Navigation." In 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE, 2021. http://dx.doi.org/10.1109/inertial51137.2021.9430487.

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Bozeman, Eric, Minhdao Nguyen, Mohammad Alam, and Jeffrey Onners. "Inertial Navigation Compensation with Reinforcement Learning." In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE, 2022. http://dx.doi.org/10.1109/inertial53425.2022.9787527.

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Stepanov, O. A., A. S. Nosov, and A. B. Toropov. "Navigation informativity of geophysical fields in map-aided navigation." In 2017 DGON Inertial Sensors and Systems (ISS). IEEE, 2017. http://dx.doi.org/10.1109/inertialsensors.2017.8171509.

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VANDERWERF, KEVIN, and KNUT WEFALD. "Fault tolerant inertial navigation system." In Digital Avionics Systems Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4024.

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Johnson, Burgess, Curt Albrecht, Todd Braman, Kevin Christ, Patrick Duffy, Daniel Endean, Markus Gnerlich, and John Reinke. "Development of a Navigation-Grade MEMS IMU." In 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE, 2021. http://dx.doi.org/10.1109/inertial51137.2021.9430466.

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Askari, Sina, Chi-Shih Jao, Yusheng Wang, and Andrei M. Shkel. "A Laboratory Testbed for Self-Contained Navigation." In 2019 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE, 2019. http://dx.doi.org/10.1109/isiss.2019.8739646.

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Endean, Daniel, Kevin Christ, Patrick Duffy, Eugene Freeman, Max Glenn, Markus Gnerlich, Burgess Johnson, and Jacob Weinmann. "Near-Navigation Grade Tuning Fork MEMS Gyroscope." In 2019 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE, 2019. http://dx.doi.org/10.1109/isiss.2019.8739669.

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Sternberg, Harald, and Matthias Fessele. "Indoor navigation with Low-Cost Inertial Navigation Systems." In 2009 6th Workshop on Positioning, Navigation and Communication (WPNC). IEEE, 2009. http://dx.doi.org/10.1109/wpnc.2009.4907796.

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Nguyen, Thanh-Le, Ying Zhang, and Martin Griss. "ProbIN: Probabilistic inertial navigation." In 2010 IEEE 7th International Conference on Mobile Ad-Hoc and Sensor Systems (MASS). IEEE, 2010. http://dx.doi.org/10.1109/mass.2010.5663779.

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Zotov, Sergey, Arvind Srivastava, Ken Kwon, Jeremy Frank, Erwin Parco, Martin Williams, Semen Shtigluz, et al. "In-Run Navigation Grade Quartz MEMS-Based IMU." In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE, 2020. http://dx.doi.org/10.1109/inertial48129.2020.9090018.

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Rapporti di organizzazioni sul tema "Inertial navigation systems"

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Kaertner, Franz X. Narrow Linewidth Tunable Solid-State Microchip Lasers for Precision Inertial Navigation Systems (PINS). Fort Belvoir, VA: Defense Technical Information Center, January 2006. http://dx.doi.org/10.21236/ada442348.

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DeMars, Kyle J., Jacob E. Darling, Michael A. Waltemate, and Samuel J. Haberberger. Performance Evaluation Criteria and Analysis of Navigation Systems Using Inertial Measurement Unit Technology. Fort Belvoir, VA: Defense Technical Information Center, June 2014. http://dx.doi.org/10.21236/ada605594.

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Ketterle, Wolfgang, Vladan Vuletic, and Mara Prentiss. Atom Interferometry on Atom Chips-A Novel Approach Towards Precision Inertial Navigation Systems (PINS). Fort Belvoir, VA: Defense Technical Information Center, May 2008. http://dx.doi.org/10.21236/ada499671.

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Habib, Ayman, Darcy M. Bullock, Yi-Chun Lin, Raja Manish, and Radhika Ravi. Field Test Bed for Evaluating Embedded Vehicle Sensors with Indiana Companies. Purdue University, 2023. http://dx.doi.org/10.5703/1288284317385.

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With the advent of modern sensing technology, mapping products have begun to achieve an unprecedented precision of measurement. Considering their diverse use cases, several factors play a role in what would make the resulting measurements accurate. For light detection and ranging (LiDAR) and photogrammetry-based mapping solutions that implement vehicles outfitted with laser ranging devices, RGB cameras, and global navigation satellite system/inertial navigation system (GNSS/INS) georeferencing units, the quality of the derived mapping products is governed by the combined accuracy of the variou
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Landherr, Stefan F., and Mark H. Klein. Inertial Navigation System Simulator: Behavioral Specification. Fort Belvoir, VA: Defense Technical Information Center, October 1987. http://dx.doi.org/10.21236/ada200604.

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Landherr, Stefan F., and Mark H. Klein. Inertial Navigation System Simulator: Behavioral Specification. Revision. Fort Belvoir, VA: Defense Technical Information Center, August 1989. http://dx.doi.org/10.21236/ada219294.

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Lee, W. S., Victor Alchanatis, and Asher Levi. Innovative yield mapping system using hyperspectral and thermal imaging for precision tree crop management. United States Department of Agriculture, January 2014. http://dx.doi.org/10.32747/2014.7598158.bard.

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Original objectives and revisions – The original overall objective was to develop, test and validate a prototype yield mapping system for unit area to increase yield and profit for tree crops. Specific objectives were: (1) to develop a yield mapping system for a static situation, using hyperspectral and thermal imaging independently, (2) to integrate hyperspectral and thermal imaging for improved yield estimation by combining thermal images with hyperspectral images to improve fruit detection, and (3) to expand the system to a mobile platform for a stop-measure- and-go situation. There were no
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Meyers, B. C., and Nelson H. Weiderman. Functional Performance Specification for an Inertial Navigation System. Fort Belvoir, VA: Defense Technical Information Center, October 1988. http://dx.doi.org/10.21236/ada204850.

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Fowler, Kenneth J. Inertial Navigation System Simulator Program: Top-Level Design. Fort Belvoir, VA: Defense Technical Information Center, January 1990. http://dx.doi.org/10.21236/ada223762.

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Brown, Alison, and Yan Lu. Indoor Navigation Test Results using an Integrated GPS/TOA/Inertial Navigation System. Fort Belvoir, VA: Defense Technical Information Center, January 2006. http://dx.doi.org/10.21236/ada458227.

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