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2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC)最新文献

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Computer-integrated navigation complex of unmanned aerial vehicles 无人机计算机集成导航综合体
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475079
V. Sineglazov, M. Filiashkin, F. M. Zaharin
{"title":"Computer-integrated navigation complex of unmanned aerial vehicles","authors":"V. Sineglazov, M. Filiashkin, F. M. Zaharin","doi":"10.1109/MSNMC.2012.6475079","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475079","url":null,"abstract":"Using inertial navigation systems and Global Positioning System together is preferable to using any of them separately. Derived benefits depend on the level of combining information.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"28 ","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134035279","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
Perspectives of integrated inertial-satellite systems development of civil aviation aircraft 民航飞机惯性卫星集成系统发展展望
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475074
V. Sineglazov, F. M. Zaharin
{"title":"Perspectives of integrated inertial-satellite systems development of civil aviation aircraft","authors":"V. Sineglazov, F. M. Zaharin","doi":"10.1109/MSNMC.2012.6475074","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475074","url":null,"abstract":"Using an inertial navigation system and Global Positioning System together is preferable to using any of them separately. Derived benefits depend on the level of combining information. Inertial navigation systems/ Global Positioning System integration architectures are defined as separate, loosely and tightly coupled, deeply integrated configurations.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"35 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133450601","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: 3
Automatic control system of low-altitude flight UAV 低空飞行无人机自动控制系统
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475117
A. P. Kozlov
{"title":"Automatic control system of low-altitude flight UAV","authors":"A. P. Kozlov","doi":"10.1109/MSNMC.2012.6475117","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475117","url":null,"abstract":"The necessity of creating automatic control low-altitude UAV flight is substantiated. Brief analyses of existing measurement tools geometric altitude of the aircraft are given. The principle of action capacitive transducer with open inhomogeneous field and its characteristic properties are considered. The results of experimental and theoretical investigations of the characteristics of a capacitive transducer are showed. Block diagrams of a system using a capacitance meter height are proposed.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"93 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122820617","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
Method of complex processing of navigation information for vehicle 车辆导航信息的复杂处理方法
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475081
L. Aniskevych, F. M. Zaharin
{"title":"Method of complex processing of navigation information for vehicle","authors":"L. Aniskevych, F. M. Zaharin","doi":"10.1109/MSNMC.2012.6475081","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475081","url":null,"abstract":"The method of processing navigation information from head-speeding and satellite navigation systems for unmannedvehicle is offered. Such method envisages the evaluation of corrections to the meterages of head and speed sensors by the iteration algorithm of nonlinear regression, and also evaluation of co-ordinates and accurate definition of corrections to the meterages of sensors with the use of generalized discrete filter.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"24 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117211734","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
Flying of the UAV by the solar energy 无人机利用太阳能飞行
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475118
K. Sydorenko, V. Budko
{"title":"Flying of the UAV by the solar energy","authors":"K. Sydorenko, V. Budko","doi":"10.1109/MSNMC.2012.6475118","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475118","url":null,"abstract":"The review of existing solar battery driven by pilots less than aircrafts has been carried out. A balance concerning energy received from the sun required for the aircraft propulsion has been made. The evaluation plot of the given index is also presented.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126138641","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
Synthesis of truncated filters in task of orientation 定位任务中截断滤波器的合成
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475098
S. I. Askerov
{"title":"Synthesis of truncated filters in task of orientation","authors":"S. I. Askerov","doi":"10.1109/MSNMC.2012.6475098","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475098","url":null,"abstract":"The question of synthesis of truncated filters in task orientation is considered. The main aim of the orientation and navigation system complexion is to increase the accuracy of determination the navigation and angular parameters of UA V orientation. The systems and separated sensors of the premier information, that generates the same parameters can be connected. During the connecting of several navigation meters, the most widely used are two schemes of complexion, that are known as the way of compensation and filtration.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"99 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122935772","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
Kalman filter stationarity analysis in the problem of INS errors estimation 卡尔曼滤波平稳性分析在惯性导航系统误差估计中的应用
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475082
I. Rataichuk, V. Kortunov
{"title":"Kalman filter stationarity analysis in the problem of INS errors estimation","authors":"I. Rataichuk, V. Kortunov","doi":"10.1109/MSNMC.2012.6475082","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475082","url":null,"abstract":"Kalman filter has long been used in aircraft integrated navigation systems as the main instrument of estimating navigation errors. Its main advantage over simpler state estimators is the ability to adjust filter's gain according to observable signal instability. But it is possible to use simple observers if filters gain is stationary regardless of aircraft maneuvers. In this paper the model of navigation errors dynamics is considered. This model is used in Kalman filer in integrated system simulation. Frequency domain representation of vehicle dynamics is used in this simulation to investigate filter stationarity. The results show that filter gain is stationary regardless of motion dynamics.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"2004 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130998421","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
Analysis of system control unmanned aerial vehicle 无人机系统控制分析
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475116
O. Ablesimov, K. Sarapina
{"title":"Analysis of system control unmanned aerial vehicle","authors":"O. Ablesimov, K. Sarapina","doi":"10.1109/MSNMC.2012.6475116","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475116","url":null,"abstract":"The principles of construction and comparative evaluation of control systems UAV is considered.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"65 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122057880","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
MEMS technology microthrusters and nanoenergetic materials for micropropulsion systems 微推进系统的MEMS技术微推力器和纳米能材料
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475111
K. Martirosyan, S. Lyshevski
{"title":"MEMS technology microthrusters and nanoenergetic materials for micropropulsion systems","authors":"K. Martirosyan, S. Lyshevski","doi":"10.1109/MSNMC.2012.6475111","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475111","url":null,"abstract":"Mini and micro air vehicles, missiles, guided munitions, projectiles and ordinances are controlled by control surfaces, thrust-vectoring and varying thrust. Microthrusters are key components of some classes of flight and naval vehicles. Solid-fuel rockets and microthrusters use solid propellants. Vehicles positioning, altitude control, orbital maneuver, aerodynamic orbit phasing and rotational manoeuvres are controlled. Enabled agility and maneuverability are achieved by advanced control schemes and propulsion systems. We examine microthrusters with solid propellants for micro- and miniature flight and naval vehicles. Fundamental, applied and experimental research and technology developments are performed by devising, designing and evaluating multi-physics MEMS technology microthrusters and propulsion systems with manoenergetic materials.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"37 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123155023","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
Non-classical conjugate vectors and polar differential equations of rotation in orientation problem 非经典共轭矢量与定向问题中旋转的极微分方程
2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC) Pub Date : 2012-10-01 DOI: 10.1109/MSNMC.2012.6475114
A. Panov, V. V. Tsysarzh
{"title":"Non-classical conjugate vectors and polar differential equations of rotation in orientation problem","authors":"A. Panov, V. V. Tsysarzh","doi":"10.1109/MSNMC.2012.6475114","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475114","url":null,"abstract":"Kinematic and dynamic differential equations of rotation of a rigid body for the \"non-classical\" conjugate three-dimensional vectors of rotation are considered in this article. The vectors modules contain tangent and cotangent of one-fourth of the rotation angle. This paper also delivers applications of the conjugate equations in the problems of orientation of a rigid body.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2012-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129616759","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
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