{"title":"Correlated Failures Analysis in Navigation System","authors":"O. Solomentsev, M. Zaliskyi","doi":"10.1109/MSNMC.2018.8576306","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576306","url":null,"abstract":"The article deals with the problem of mathematical modeling of correlated vector of failures that can occur in navigation system. The modeling problem is considered for the case of two-dimensional distribution. This distribution corresponds to the event, when failure of whole navigation system occurs only in case of simultaneous failures of two structural units of the system. The article presents several methods of exponential correlated field formation. The modeling results can be used in case of design of operation strategy according to the condition with control of diagnostic variables to determine the optimal time interval for preventive maintenance action realization.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"154 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131325809","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Setting the PID Controller for Controlling Quadrotor Flight: a Gradient Approach","authors":"D. Kucherov, A. Kozub, A. Rasstrygin","doi":"10.1109/MSNMC.2018.8576294","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576294","url":null,"abstract":"The paper deals with the design of an autopilot for a quadrotor based on a PID controller. A mathematical description of the control object in form of the system of second-order differential equations is also presented. Setting the parameters of the PID controller is an iterative procedure. The paper investigates three optimal tuning algorithms based on minimizing the quality integral: coordinate descent, gradient descent, and steepest descent. During the research, a number of advantages of the gradient search algorithm are established. Gradient search is used as the main design method; on its basis, the autopilot model is synthesizing. Some simulation results are presented, which are confirmed by the Simulink autopilot model.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"29 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129814327","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Power Efficient Combined Heat Supply System for Ground Navigation Equipment","authors":"S. Tovkach, M. Kravchuk, T. Kravchuk","doi":"10.1109/MSNMC.2018.8576303","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576303","url":null,"abstract":"The new power efficient combined heat supply system, which combines five circuits of the heat supply system namely the contour of the solar collector, the boiler circuit, the pyrolysis and gas boiler circuit, the heating system circuit and the hot water supply circuit has been considered; the efficiency of the combined heat supply system operation depending on the temperature in each circuit and the efficiency of the solar collectors, operating modes of the gas and pyrolysis boilers has been investigated.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"5 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130768009","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
V. Konin, O. Kutsenko, E. O. Lukianenko, S. Ilnytska
{"title":"Experimental Investigation of Multi-GNSS in Static Mode","authors":"V. Konin, O. Kutsenko, E. O. Lukianenko, S. Ilnytska","doi":"10.1109/msnmc.2018.8576274","DOIUrl":"https://doi.org/10.1109/msnmc.2018.8576274","url":null,"abstract":"The results of multi-GNSS, including Global Positioning System, GLONASS, GALILEO and BEIDOU, experimental investigation are presented in a paper. Accuracy characteristics, mean square deviations for various cases of multi-GNSS and type of approach are provided with analysis regarding possibility of global navigation satellite system use at the considered moment of time.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121751531","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
O. Sushchenko, V. Golitsyn, O. Krivonosenko, S. D. Egorov
{"title":"Improvement of Inertial Sensors for Using in Stabilization Systems","authors":"O. Sushchenko, V. Golitsyn, O. Krivonosenko, S. D. Egorov","doi":"10.1109/MSNMC.2018.8576312","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576312","url":null,"abstract":"The paper deals with consideration of the possibility to improve the Coriolis vibratory gyroscopes with the goal to simplify information processing, increase reliability, and compensate bias. Improvement of the Coriolis vibratory gyroscope includes introducing of the phase detector and additional excitation unit. The possibility to use the improved Coriolis vibratory gyroscope in the stabilization system is shown by means of simulation technique.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"19 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121133745","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Synthesis of an Optimal Stochastic Stabilization System for an Unstable Multivariable Object with Time Delays in Controls","authors":"S. Osadchy, V. Zubenko, M. Fedotova","doi":"10.1109/MSNMC.2018.8576321","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576321","url":null,"abstract":"In the work, the problem of developing the method for synthesizing an optimal multidimensional discrete stabilization system of an object with delays in controls that operates under the influence of multidimensional stationary random useful signals, disturbances and measurement noises has been posed and solved. This method differs in that it allows instability of the control object, various delays in the components of the control signal vector, the imperfection of the sensors in the stabilization system, simplification of the synthesis algorithm with respect to the known one.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"59 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129499534","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Double Optimal Processing of Multilateration Surveillance System Measurements to Improve Aircraft Tracking","authors":"V. Vasyliev, D. Vasyliev, K. V. Naumenko","doi":"10.1109/MSNMC.2018.8576302","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576302","url":null,"abstract":"The method for improving the performances of aircraft tracking by double sequential optimal processing of multilateration surveillance system data is proposed.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130901674","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Combined Symmetry of Exponential and Extreme Hyperbolic Distributions in Macrosystems","authors":"M. Delas","doi":"10.1109/MSNMC.2018.8576264","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576264","url":null,"abstract":"An extended entropy method has been developed that accounts for the finite properties of distributions and the stagewise character of relaxation processes. The kinetic properties of system agents (carriers and resources) determine the distribution type. If the time of relaxation of carriers is shorter, the exponential distribution is formed, whereas if the dynamic resources are more agile, an extreme heavy-tail hyperbolic distribution is formed. The exponential and extreme hyperbolic distributions have been found to possess combined symmetry, which is a different statistical interpretation of a single state.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"47 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134046626","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Model of Analysis LIDAR’s 3D Images for Survey-Comparative Navigation Systems","authors":"O. Chuzha","doi":"10.1109/MSNMC.2018.8576279","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576279","url":null,"abstract":"The location’s determination of an airplane by survey-comparative methods navigation means the identification of landmarks and their correspondence to the standard image with known coordinates. The geometric characteristics of ground landmarks are determined most accurate by the simulation of their features when processing 3D images of LIDAR.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129354296","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Analysis of Solar Rechargeable Airplane","authors":"D. Karabetsky, V. Sineglazov","doi":"10.1109/MSNMC.2018.8576181","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576181","url":null,"abstract":"In this paper, main goal focused on analysis for solar rechargeable airplane. This analysis has in configuration flow parameters that represent time and location of the starting point, solar cells performance and surface area, energy storage characteristics with initial state and power distribution for on-board systems. Simulation provides full continuous flight day performance for available power acquired from the Sun during the flight time, required power that unmanned aerial vehicle actually use and on-board battery bank’s state of charge.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"194 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132071168","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}