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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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Simulator training optimization of UAV external pilots 无人机外聘飞行员模拟器训练优化
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979734
Ju. M. Shmelev
{"title":"Simulator training optimization of UAV external pilots","authors":"Ju. M. Shmelev","doi":"10.1109/MSNMC.2014.6979734","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979734","url":null,"abstract":"The process of unmanned aerial vehicle external pilots training by simulator is considered. It is analyzed the aviation accidents due to human factor. It is proposed the way of estimation of unmanned aerial vehicle external pilots training efficiency in the simulator.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"57 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":"126694586","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
Output measurement unit signal integration process research of antenna stabilization system 天线稳定系统输出测量单元信号集成过程研究
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979764
L. Ryzhkov, M. V. Ozhoh, O. Prokopovych
{"title":"Output measurement unit signal integration process research of antenna stabilization system","authors":"L. Ryzhkov, M. V. Ozhoh, O. Prokopovych","doi":"10.1109/MSNMC.2014.6979764","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979764","url":null,"abstract":"Usage of micromechanical angular rate measurement device as an antenna stabilization system sensitive element is considered. Namely-collecting data of orientation for holding direction at an object within referenced accuracy limits and during certain period of time.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"30 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":"114283572","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
Analytical model of air navigation system operator reliability 空中导航系统操作员可靠性分析模型
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979761
O. Kozhokhina, V. Gribov, S. I. Rudas
{"title":"Analytical model of air navigation system operator reliability","authors":"O. Kozhokhina, V. Gribov, S. I. Rudas","doi":"10.1109/MSNMC.2014.6979761","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979761","url":null,"abstract":"This paper deals with operator's reliability and optimal analytical model as the basis of estimation of operator's errors distribution. The mail goal is to determine the operator's reliability by the means of the chosen model. Peculiarities of reliability models were discovered and the most appropriate one was chosen according to the requirements and calculation advantages. Method of diffusion nonmonotonic model calculation is performed.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"88 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":"114765647","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
Differential CVG shock damping capacity computer simulation results 差分CVG减震能力的计算机模拟结果
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979751
V. Chikovani, H. Tsiruk
{"title":"Differential CVG shock damping capacity computer simulation results","authors":"V. Chikovani, H. Tsiruk","doi":"10.1109/MSNMC.2014.6979751","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979751","url":null,"abstract":"This work presents investigation of differential Coriolis vibratory gyroscope ability to external shock suppression. First of all pulse amplitude in voltage caused by external mechanical shock of 100 g is estimated for the two sensor designs. Then, using differential CVG Simulink model, output signals of two channels are analyzed. It is shown that differential CVG damps amplitude of erroneous angle rate caused by shock directed along sensing axis of no less than 3 times in comparison with non differential CVG. As to lateral shock both CVGs have equal damping capacities.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"57 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":"114853234","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
Control of dynamic processes of navigation systems function states 导航系统功能状态动态过程控制
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979724
V. Chepizhenko, O. Tryzna
{"title":"Control of dynamic processes of navigation systems function states","authors":"V. Chepizhenko, O. Tryzna","doi":"10.1109/MSNMC.2014.6979724","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979724","url":null,"abstract":"This paper deals with a problem of aircraft navigation systems components condition change forecasting, which is connected with lack of admissible approaches and methods. The solution of the problem lies in development of models taking into account the unit condition change, caused by either operating time, or service period. The goal of the paper is determination of requirements to aircraft maintenance work volume and content, and also.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"38 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":"124576947","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
Particle filtering in complex correlation-extremal navigation 复杂相关极值导航中的粒子滤波
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979727
M. Mukhina
{"title":"Particle filtering in complex correlation-extremal navigation","authors":"M. Mukhina","doi":"10.1109/MSNMC.2014.6979727","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979727","url":null,"abstract":"Problem of correlation-extremal navigation for several geophysical fields is considered. Optimal estimation for highly non-linear measurement equation is realized using particle filtering. Simulation for relief and anomalous magnetic fields is done by sequential importance sampling based on Monte Carlo method.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"2 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":"134343497","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
The dynamic validation of the three-component microelectromechanical speed gyro 三分量微机电速度陀螺的动态验证
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979762
M. Melnychenko, O. Didyk, O. Serbul
{"title":"The dynamic validation of the three-component microelectromechanical speed gyro","authors":"M. Melnychenko, O. Didyk, O. Serbul","doi":"10.1109/MSNMC.2014.6979762","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979762","url":null,"abstract":"The article presents a method of validation the three-component microelectromechanical speed gyro which will later be used in the design of an automated navigation system working body of the machine-hexapod.","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":"129331051","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
Operative programming method of flight route 航路操作规划方法
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979738
N. F. Tupitsin
{"title":"Operative programming method of flight route","authors":"N. F. Tupitsin","doi":"10.1109/MSNMC.2014.6979738","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979738","url":null,"abstract":"The paper presents description algorithm of the trajectory motion correction of an aircraft. The part operations of algorithm are shown in detail. Example of calculation of returning the aircraft to a predetermined route line is given.","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":"121475356","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
Features of control by two-axis gimbaled attitude and heading reference system 两轴平衡姿态和航向参考系统控制的特点
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979766
O. Sushchenko
{"title":"Features of control by two-axis gimbaled attitude and heading reference system","authors":"O. Sushchenko","doi":"10.1109/MSNMC.2014.6979766","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979766","url":null,"abstract":"This paper deals with autonomous precision attitude and heading reference system. Usage of the dynamically tuned gyros and two-axis gimbals that allows to reduce mass and dimensions of the studied system is suggested. The model of the studied system is given. Forming of the control moments is considered.","PeriodicalId":360002,"journal":{"name":"2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"140 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":"130309111","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
Automation of aircraft control reconfiguration in flight special situations 飞行特殊情况下飞机控制重构的自动化
2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2014-12-11 DOI: 10.1109/MSNMC.2014.6979759
V. Kazak, V. Vovk, D. Shevchuk, M. Levchenko
{"title":"Automation of aircraft control reconfiguration in flight special situations","authors":"V. Kazak, V. Vovk, D. Shevchuk, M. Levchenko","doi":"10.1109/MSNMC.2014.6979759","DOIUrl":"https://doi.org/10.1109/MSNMC.2014.6979759","url":null,"abstract":"The paper explains the possibility of applying the system of parametric methods, structural reconfiguration control and reconfiguration of the object control objectives to prevent the transition to the current flight situation into a catastrophic one and maintain the specified level of safety. The article presents a block diagram of a control system developed reconfigurable dynamic system, and describes how it works.","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":"121763244","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: 7
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