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2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)最新文献

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Method of sequential estimation of statistical distribution parameters in control systems design 控制系统设计中统计分布参数的顺序估计方法
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979752
O. Solomentsev, M. Zaliskyi
{"title":"Method of sequential estimation of statistical distribution parameters in control systems design","authors":"O. Solomentsev, M. Zaliskyi","doi":"10.1109/MSNMC.2014.6979752","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979752","url":null,"abstract":"The paper presents one method of sequential parameter estimation of probability distribution. Equations for theoretical probability distribution function, mathematical expectation and variance of estimates and observation duration are given in the article.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"23 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125920793","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}
引用次数: 30
Navigation and orientation system with optical horizon sensor for mini UAV 小型无人机光学地平传感器导航定位系统
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979717
A. Zbrutsky, J. A. Malysheva, V. Burnashev
{"title":"Navigation and orientation system with optical horizon sensor for mini UAV","authors":"A. Zbrutsky, J. A. Malysheva, V. Burnashev","doi":"10.1109/MSNMC.2014.6979717","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979717","url":null,"abstract":"National Technical University of Ukraine “Kyiv Polytechnic Institute” develops and offers unmanned aerial vehicles for using in many areas of civil and military applications.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129467381","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}
引用次数: 4
Optimal filtering of hexapod acceleration data obtained under action of electromagnetic interference 电磁干扰作用下六足加速度数据的最优滤波
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979719
S. Osadchy, V. Zozulya
{"title":"Optimal filtering of hexapod acceleration data obtained under action of electromagnetic interference","authors":"S. Osadchy, V. Zozulya","doi":"10.1109/MSNMC.2014.6979719","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979719","url":null,"abstract":"The algorithms of the synthesis of optimal structures and parameters of the matrix of transfer functions of the filter which enables to assess the vector of useful signals with the noise correction as well as without it according to the data on sensor dynamics, electromagnetic interference characteristics and vector characteristics of the measured signals were developed.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132600318","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}
引用次数: 0
Synthesis of two-degree-of-freedom system for stabilization of information-measuring devices on moving base 移动基座上信息测量装置稳定的二自由度系统综合
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979756
O. Sushchenko
{"title":"Synthesis of two-degree-of-freedom system for stabilization of information-measuring devices on moving base","authors":"O. Sushchenko","doi":"10.1109/MSNMC.2014.6979756","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979756","url":null,"abstract":"The problem of design of the robust combined systems for stabilization and control by orientation of lines-of-sight of devices mounted at vehicles in difficult conditions of real operation is considered. The optimization criterion of the solved problem taking into consideration the functions of sensitivity by the coordinate disturbances and noise measurements is obtained.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"20 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128823343","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}
引用次数: 4
Whole angle force rebalance control for coriolis vibratory gyroscopes 科氏振动陀螺仪的全角力再平衡控制
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979730
V. Apostolyuk
{"title":"Whole angle force rebalance control for coriolis vibratory gyroscopes","authors":"V. Apostolyuk","doi":"10.1109/MSNMC.2014.6979730","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979730","url":null,"abstract":"Synthesis of a feedback control system for Coriolis vibratory gyroscopes that implements whole angle force rebalance mode of operation is presented in this paper. Feedback controller is derived in terms of demodulated signals. Successful operation of the control system is demonstrated using numerical simulation of realistic Coriolis vibratory gyroscopes model in modulated signals.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"6 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114891201","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}
引用次数: 2
Recommendations to UAV navigation system test validation and some practical results 对无人机导航系统的试验验证提出了建议，并取得了一些实际效果
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979723
V. Kharchenko, V. Kondratyuk, S. Ilnytska, O. Kutsenko
{"title":"Recommendations to UAV navigation system test validation and some practical results","authors":"V. Kharchenko, V. Kondratyuk, S. Ilnytska, O. Kutsenko","doi":"10.1109/MSNMC.2014.6979723","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979723","url":null,"abstract":"Unmanned aerial vehicles (UAV) are successfully exploited in different applications for the last years. To perform successfully the specified tasks they have to rely on navigation and automatic flight control systems. Development of such systems is a complex task that requires comprehensive testing throughout the whole process. This paper presents some recommendations regarding UAV navigation system test validation and some results from the flight experiment approving integrated navigation system efficiency of functioning.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"469 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123245769","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}
引用次数: 12
Optimal flight control system design via LMIs 基于lmi的飞行控制系统优化设计
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979758
M. Komnatska
{"title":"Optimal flight control system design via LMIs","authors":"M. Komnatska","doi":"10.1109/MSNMC.2014.6979758","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979758","url":null,"abstract":"The problem of optimal state feedback controller design in terms of quadratic performance index is considered. The problem is formulated in the form of linear matrix inequalities (LMIs). The obtained solution guarantees stabilization of the aircraft during flight mission. During flight envelope the aircraft is subjected to the external stochastic disturbances. The efficiency of the proposed approach is illustrated by a case study of airplane longitudinal motion.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"87 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123831438","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}
引用次数: 1
Combined sensor of angular parameters for small unmanned aerial vehicles 小型无人机角参数组合传感器
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979729
M. Filyashkin
{"title":"Combined sensor of angular parameters for small unmanned aerial vehicles","authors":"M. Filyashkin","doi":"10.1109/MSNMC.2014.6979729","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979729","url":null,"abstract":"Are given principles of the combined sensor which measures the angular parameters and is used in inertial-satellite systems constructed by the method of compensation or based on the reduced Kalman filter. Measurement errors of angular orientation parameters are investigated by the proposed method with aircraft performing various maneuvers and with changing the acceleration and attitude.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"70 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123935657","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}
引用次数: 0
Mathematical description of phenomenon of amplification of integral-differential motive dynamic stereotype 积分-微分动力刻板印象放大现象的数学描述
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979733
Y. Hryshchenko, A. Skripets, V. Tronko
{"title":"Mathematical description of phenomenon of amplification of integral-differential motive dynamic stereotype","authors":"Y. Hryshchenko, A. Skripets, V. Tronko","doi":"10.1109/MSNMC.2014.6979733","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979733","url":null,"abstract":"This paper describes the correlation functions between the information on the flight path and distortions in the tracking operations of operator. This is due to its psychophysiological abilities in a state of high tension.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"32 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128695108","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}
引用次数: 1
Landmarks navigation system software 地标导航系统软件
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979731
V. Sineglazov
{"title":"Landmarks navigation system software","authors":"V. Sineglazov","doi":"10.1109/MSNMC.2014.6979731","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979731","url":null,"abstract":"The structural scheme of landmarks navigation system for unmanned aerial vehicles is developed. It is supposed the algorithm of this system. The software of landmarks navigation system is developed.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"32 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121962525","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}
引用次数: 5
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