{"title":"Inertial Measurement Unit and External Influence Duration","authors":"Y. Opanasiuk","doi":"10.1109/MSNMC.2018.8576284","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576284","url":null,"abstract":"After a short discussion of the main specific points of existing air navigation schemes with relation to external disturbing influences, some new approach to analyze in the view of admissible temporal and spatial frames basic principle on which the simplest accelerometer may be constructed is proposed. It is shown that a strict successive analysis of accelerometer measurement procedure makes it possible to understand probable new source of errors in the value estimation of the disturbing force magnitude. If do not take into account these new possible errors any self-adjusting system of an airplane may be functionally unreliable. These errors arise only when temporal duration of disturbing force is less than some critical time τ, which depends on the given characteristics of an aircraft Inertial Navigation System and aircraft itself. The method of finding τ is proposed.","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":"133861505","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":"Active Systems Communicational Control Assessment in Multi-Alternative Navigational Situations","authors":"A. Goncharenko","doi":"10.1109/MSNMC.2018.8576285","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576285","url":null,"abstract":"The paper goal is to investigate the influence of a communicative networking upon the navigation control and managerial decision making process in the framework of the subjective entropy maximum principle. The subjective analysis theory entropy paradigm makes it possible to consider the navigation control system based upon communication networks as an active system governed by an individual (active element of the control system) with the help of her/his individual subjective preferences optimal distributions obtained in conditions of operational multi-alternativeness and, those navigation operational alternatives, the active system active element’s individual subjective preferences uncertainty. The described approach takes into account the simple navigational two-alternative operational situation in regards with the objectively existing effectiveness functions, related to informative communication, in the view of a controlled parameter and a combination of it with its rate as the product. The obtained expressions for the objective functional extremal functions of the effectiveness and preferences, as well as the subjective entropy of the alternatives preferences, illustrated in diagrams, visualize the navigational situation and allow taking a good choice. The ideas of the required proper governing, managing, and control methods choice optimization with respect to only 2 alternative navigational objective effectiveness functions arguments might be simple; nevertheless, increasing the number of motion control parameters and further complication of the problem setting will not change the principle of the problem solution.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"36 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":"114284805","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":"Evaluation of Quality and Accuracy of Flight Path During Approach and Landing","authors":"Y. Hryshchenko, V. Romanenko, D. Pipa","doi":"10.1109/MSNMC.2018.8576171","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576171","url":null,"abstract":"The article deals with the problem related to the assessment of the deterioration of the piloting technology’s quality under the influence of negative factors. The methods of training for solving this problem are considered. A method for determining this tendency by the boundaries designated in space is proposed. The quality of landing depends on the accuracy of all stages of landing. The method of analysis and estimation of the quality of the approaching to the glide path in three-dimensional coordinate system is proposed.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"102 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":"114324719","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}
Roman Voliansky, Oleksander Sadovoi, Nina Volianska
{"title":"Defining of Lyapunov Functions for the Generalized Nonlinear Object","authors":"Roman Voliansky, Oleksander Sadovoi, Nina Volianska","doi":"10.1109/MSNMC.2018.8576315","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576315","url":null,"abstract":"The paper d eals with the development of a method for defining of Lyapunov functions. This method is based on usage of coordinate transformations for both linear and nonlinear dynamical objects. One can use proposed method for definition of Lyapunov functions, which can be used as a basis for stability analysis. Positiveness and continuity of the above-mentioned functions are guaranteed by using the complete square technique while coefficients of Lyapunov functions are defined. Lyapunov functions which are defined into such way can be converted into various state spaces. Such transformation allows us to get non-quadratic Lyapunov functions for nonlinear dynamic objects and quadratic for linear ones. While one use Lie derivatives for performing coordinate transformation he can reduce the order of Lyapunov function, which is obtained for a controllable dynamical object.","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":"115678129","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":"Local Polarimetric Aviation Navigation System","authors":"A. Klochan, A. Al-Ammouri, V. Kharuta, L. Osipa","doi":"10.1109/MSNMC.2018.8576288","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576288","url":null,"abstract":"The paper considers questions of invention the local optical navigation system on base on polarimetric technologies. Such system is aimed to increase the sensitivity and accuracy of definition the aircraft navigation and piloting parameters in a locally restricted airspace segment with high traffic density. The paper also deals with regarding existing methods and systems for measuring the aircraft’s piloting and navigation parameters and suggest polarimetric navigation method and the local polarimetric navigation system, that realize it. The paper is provided the result of mathematical modeling of system operation and is described dependencies for estimation the navigation and piloting parameters.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"18 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":"124392440","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":"Automated Algorithmic Procedure of Robust-Optimal Control System’s Synthesis for Marine Vehicles","authors":"V. Timchenko, D. O. Lebedev","doi":"10.1109/MSNMC.2018.8576265","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576265","url":null,"abstract":"The article presents the results of the development of an automated procedure for the synthesis of algorithms for variable structures of the robust-optimal control of the movement of a marine vehicle in the context of incomplete information on the parameters of a multidimensional nonlinear model of the object and external disturbances. The results of modeling the developed algorithms for the stabilization processes of the marine vehicle on a complex trajectory with the required accuracy are presented.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"22 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":"125065314","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. Kazak, D. Shevchuk, L. V. Panchuk, V. V. Shulevka
{"title":"Methods and Tools for Evaluating the Accuracy of the Air Navigation Using GNS","authors":"V. Kazak, D. Shevchuk, L. V. Panchuk, V. V. Shulevka","doi":"10.1109/MSNMC.2018.8576273","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576273","url":null,"abstract":"The development of the global satellite navigation system enabled not only to set more stringent requirements for flight tracks, optimization of arrival and departure, but also gave impetus to the creation of new methods for determining the accuracy of navigation systems.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"86 6 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":"127991814","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}
S. Shvorov, D. Komarchuk, N. Pasichnyk, O. Opryshko, Y. Gunchenko, S. Kuznichenko
{"title":"UAV Navigation and Management System Based on the Spectral Portrait of Terrain","authors":"S. Shvorov, D. Komarchuk, N. Pasichnyk, O. Opryshko, Y. Gunchenko, S. Kuznichenko","doi":"10.1109/MSNMC.2018.8576304","DOIUrl":"https://doi.org/10.1109/MSNMC.2018.8576304","url":null,"abstract":"The paper is devoted to research on unmanned aerial vehicle navigation using spatial-spectral portraits of the terrain. Such navigation is relevant in the event of failure of global positioning system receivers and other navigation equipment, but its implementation requires the solution of a number of methodological issues. In particular, the effect of illumination changes on the spectral characteristics of objects should be taken into account. The borrowing of satellite solutions using optical patterns is inadequate for low-flying unmanned aerial vehicles and it is more promising to use the service data from the meter display of the spectral sensory equipment of the unmanned aerial vehicle. In this research, an existing method for correction of illumination changes based on the value of LightValue for different cameras in laboratory and field conditions is considered. It has been experimentally established that the dependencies between LightValue and the intensities of color constituents in different cameras are individual in nature. For the correction due to changes in natural light, it is suggested to use experimentally obtained dependences for specific brands of the sensory equipment. When organizing navigation systems for spectral portraits of the terrain, it is recommended to use objects with the most stable optical changes in terms of illumination.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"40 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":"125937435","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}