{"title":"Use of Kalman filter in orientation systems","authors":"S. I. Askerov","doi":"10.1109/MSNMC.2012.6475096","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475096","url":null,"abstract":"The use of Kalman filter in system of orientation is considered. The block diagrams and Kalman filter realization is proposed.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"15 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":"121027090","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":"Whole angle approximations of aerodynamic coefficients","authors":"Z. V. Didyk, V. Apostolyuk","doi":"10.1109/MSNMC.2012.6475107","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475107","url":null,"abstract":"This paper addresses the whole angle approximations of aerodynamic coefficients. Several nonlinear approximations are proposed to describe lift, drag and side force coefficients in the range from 0 to 360 degrees based on accuracy and simplicity.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"18 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":"117196252","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":"State space identification of flight dynamics models","authors":"A. M. Klipa","doi":"10.1109/MSNMC.2012.6475108","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475108","url":null,"abstract":"This paper is devoted to the state space identification of the flight dynamics models in the presence of sensor noise and biases. The goal of the identification procedure is not only the estimation aircraft stability and control derivatives, but also the biases of sensors. It is achieved by using the procedure of the likelihood function minimization, based on the Kalman filter and the stochastic approximation procedure. The application technique of the least-squares method to a state space model in order to determine initial values of unknown parameters which are necessary to identify the state space model by maximum likelihood method is created. This procedure was used for state space identification of the model of lateral-directional dynamics of small 6-seat aircraft and results of this identification are presented.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"144 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":"131592489","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":"Least squares criterion using to improve the TRIAD algorithm","authors":"L. Ryzhkov, D. I. Stepurenko","doi":"10.1109/MSNMC.2012.6475103","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475103","url":null,"abstract":"In this paper a using of least squares criterion is proposed to reduce the measurement errors influence to the TRIAD algorithm accuracy. The method testing was carried out to verify the proposed formulas. The case of constant attitude was considered and the results of its estimation are presented.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"19 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":"122323700","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":"Application of exceptional non-normalized quaternions, five-dimensional rotation vectors and their algebras in problems of inertial orientation","authors":"A. Panov, V. V. Tsysarzh","doi":"10.1109/MSNMC.2012.6475113","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475113","url":null,"abstract":"Exceptional non-normalized quaternions, five-dimensional rotation vectors (pentanions) and their algebras in problems of inertial orientation are considered in this article.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"162 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":"126741347","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":"Nonlinear analysis and tracking control of advanced airframe aircraft","authors":"A. S. Chauhan, S. Lyshevski","doi":"10.1109/MSNMC.2012.6475075","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475075","url":null,"abstract":"This paper focuses on nonlinear dynamics, optimization and control of longitudinal and lateral dynamics of flight vehicles. For advanced airframes and multiple control surfaces, it is impossible to linearize and decouple longitudinal and lateral dynamics. Nonlinear analysis and control are performed. For a given enabling airframe and control schemes, a robust design concept is researched. A consistent design is applied with a minimum level of simplifications and assumptions. Our findings are verified and demonstrated for practical problems. The reported design enables near-real-time implementation due to conceptual consistency, robustness, computational efficiency and algorithmic effectiveness. The proposed concept is effective in design of flight control and management systems.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"70 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":"131777680","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":"Theoretical framework to costruct optimal flight safety diagnostic procedures","authors":"Y. Opanasiuk","doi":"10.1109/MSNMC.2012.6475083","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475083","url":null,"abstract":"The problem of reconstruction of the avionic equipment diagnostic procedures to meet the new challenges is discussed. After short review of the essentials of the modern Information and Optimal Control theories ways of their applications in the framework of proposed mathematical formalism are described.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"13 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":"123629945","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":"Simulator as a teaching system","authors":"S. Borsuk","doi":"10.1109/MSNMC.2012.6475084","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475084","url":null,"abstract":"Modern aviation simulators are commonly used in training aircraft crew and land service employees. The need to provide qualitative education makes the aviation simulators modify in their structure using algorithms and their elements. Thus it is very important to pay attention to simulators from the other side - using them for teaching.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"23 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":"115398654","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 delays encountered in control of UAV","authors":"R. Tkachov, V. Sineglazov","doi":"10.1109/MSNMC.2012.6475115","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475115","url":null,"abstract":"The causes of delays in the control circuit of UAV are considered. The necessity of taking into high-speed performance, memory and capacity of digital hardware facilities, realizing the system of autonomous remote control is substantiated.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"5 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":"130086770","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":"Aircraft's trajectory in the compressed time scale prediction as the flight control on-board systems intellectualization","authors":"O. Melnykov, N. Apenko, O. Gaydamaka","doi":"10.1109/MSNMC.2012.6475085","DOIUrl":"https://doi.org/10.1109/MSNMC.2012.6475085","url":null,"abstract":"The paper examines approaches to solving the problem of improving the effectiveness and aircraft safety based on the methodology of predictive modeling of the aircraft flight path on a compressed time scale on the CWU board.","PeriodicalId":394899,"journal":{"name":"2012 2nd International Conference \"Methods and Systems of Navigation and Motion Control\" (MSNMC)","volume":"32 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":"121460197","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}