{"title":"Intelligent system for visual navigation","authors":"V. Sineglazov, V. Ischenko","doi":"10.1109/MSNMC.2016.7783094","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783094","url":null,"abstract":"In this article it is considered the problem of algorithmic maintenance for visual navigation system. It is analyzed the characteristic features of different methods of intelligent system synthesis for visual navigation. The main stages and algorithms of work visual navigation system are encouraged to develop algorithmic maintenance for intellectual visual navigation system based on convolution neural networks.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"14 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122640763","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. Chikovani, H. Tsiruk, A. Beregovoy, V. Makarenko, V. G. Paraschanov
{"title":"Influence of external acoustic disturbances on differential vibratory gyroscope output signals","authors":"V. Chikovani, H. Tsiruk, A. Beregovoy, V. Makarenko, V. G. Paraschanov","doi":"10.1109/MSNMC.2016.7783115","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783115","url":null,"abstract":"Test results on the influence of periodic and noisy acoustic disturbances on differential metallic resonator Coriolis vibratory gyroscope which resonant frequency is close to frequency of periodic acoustic disturbances are presented in this paper. Small sensitivities to noisy acoustic disturbances of 100 dB intensity in the frequency range of 1-10 kHz that covers resonant frequency have been revealed both for differential and non differential channels of differential vibratory gyro. No any influence on differential CVG output signals under action of periodic acoustic disturbances close to resonant frequency has been revealed.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"19 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124091464","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":"Several models of artificial intelligence elements for airctaft control","authors":"A. Goncharenko","doi":"10.1109/MSNMC.2016.7783148","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783148","url":null,"abstract":"It is made an attempt to find some optimal measure for the coefficient of a proportional governor augmentation in the aircraft navigation and motion linear model inertness-less object control system as continuous alternatives individual preferences densities distributions, using the preferences subjective entropy maximum principle, proposed by Professor V.A. Kasianov (National Aviation University, Kyiv, Ukraine) in case of one and two-dimensions. It is obtained the continuous alternative preferences distribution densities; this together with the preferences distributions for the predetermined time points allows making the optimal choice of the available aircraft navigation. Theoretical speculations are illustrated with the example calculation experiments. The necessary diagrams are plotted.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"13 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127559443","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":"Identification of the signals in position control circuits of a hexapod platform","authors":"M. Melnichenko, S. Osadchy, V. Zozulya","doi":"10.18372/1990-5548.50.11387","DOIUrl":"https://doi.org/10.18372/1990-5548.50.11387","url":null,"abstract":"The paper deal method of identification useful signals, the disturbance and interference operating hexapod platform management system for modeling large-scale marine spatial pitching ship.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132706703","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":"Algorithm of attitude determination using vectors measurements","authors":"L. Ryzhkov","doi":"10.1109/MSNMC.2016.7783114","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783114","url":null,"abstract":"The algorithm of attitude determination based on geometric relations and least-square method is proposed. The algorithm is based on Gibbs vector using. The analysis of accuracy of the proposed algorithm is fulfilled. It was shown that if the angle of body's turn doesn't equal 180° the accuracy of proposed algorithm is equivalent to the accuracy of algorithm QUEST.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"113 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133527310","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":"Optimal stabilization system analysis of unstable multivariate movable object","authors":"S. I. Osadchii, I. Prokofieva","doi":"10.1109/MSNMC.2016.7783136","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783136","url":null,"abstract":"The paper describes the way to improve control accuracy of the unstable multivariate movable object with the help of optimal controller synthesis; also there is performance comparison between the system with optimal controller and the regular one.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"319 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116105358","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. Pavlova, L. Blahaia, O. Kozhokhina, T. Herasymenko
{"title":"Model of side-looking airborne radar controller activity","authors":"S. Pavlova, L. Blahaia, O. Kozhokhina, T. Herasymenko","doi":"10.1109/MSNMC.2016.7783107","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783107","url":null,"abstract":"The paper deals with the air navigation system and indicated the location of the human-operator as an element of radar system. Additionally the model of side-looking airborne radar operator activities is proposed. The possibilities of queuing system application for the creation of mathematical model human-operator are described.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124049908","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}
Y. Gunchenko, S. Shvorov, Nickolay Rudnichenko, V. Boyko
{"title":"Methodical complex of accelerated training for operators of unmanned aerial vehicles","authors":"Y. Gunchenko, S. Shvorov, Nickolay Rudnichenko, V. Boyko","doi":"10.1109/MSNMC.2016.7783124","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783124","url":null,"abstract":"The paper propose methodical complex and approach to organization process of accelerated training for unmanned aerial vehicles operators. This approach provide procedure of operator training to the required level at a low cost and in a short time. Basic objectives, principles of construction and organization of system's operation for intensive training in a short time and at low costs provides training of unmanned aircraft operators described.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"30 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122718896","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":"System of the monitoring the aircraft construction in the tests process","authors":"A. P. Kozlov, A. Yurchenko","doi":"10.1109/MSNMC.2016.7783119","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783119","url":null,"abstract":"The necessity of the organization and implementation of continuous monitoring of deformations in the dements of the aircraft construction for the early detection of critical values is shown. The short review of existing methods and devices for measuring micro-movements is given. Variants of designs of micro-movements sensors are considered and a block diagram of a measuring instrument, which was built on the basis of a capacitive transducer with an “open” field, is given. The functioning of the system of non-contact measurement of deformation elements of the aircraft structure is considered.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"2230 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130187240","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":"Minimum landing speed criteria generated by means of avionics","authors":"O. Chuzha","doi":"10.1109/MSNMC.2016.7783159","DOIUrl":"https://doi.org/10.1109/MSNMC.2016.7783159","url":null,"abstract":"This paper deal with stall warning system critical flight modes. Special focus was on critical conditions warning indication during landing. Recommendations about the basic parameters required for display warning critical conditions whilst landing was proposed.","PeriodicalId":420538,"journal":{"name":"2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"74 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128383053","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}