A. Skripets, A. G. Sytnyk, A. A. Polozhevets, M. O. Onyshchuk
{"title":"Optimal aerospace monitoring by means of UAV intelligent control","authors":"A. Skripets, A. G. Sytnyk, A. A. Polozhevets, M. O. Onyshchuk","doi":"10.1109/APUAVD.2013.6705319","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705319","url":null,"abstract":"The paper deals with the theoretical aspects of unmanned aerial vehicle intelligent control efficiency estimation. The avionics systems efficiency and criteria of its evaluation are analysed. Distinguishing of avionics systems efficiency and criterions of its evaluation is carried out.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"21 6","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133586840","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":"Flying wing design for solar rechargeable aircraft","authors":"V. Sineglazov, D. P. Karabetsky","doi":"10.1109/APUAVD.2013.6705281","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705281","url":null,"abstract":"This paperwork proposes a methodology to design a flying wing for solar aircraft on complex basis.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"136 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134463987","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":"Integrated aircraft navigation system","authors":"J. Malysheva","doi":"10.1109/APUAVD.2013.6705316","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705316","url":null,"abstract":"The paper describes the integrated aircraft navigation system, which includes the strapdown inertial navigation system (SINS), GPS receiver, optical horizon sensor and magnetometer. The integration algorithm for such system based on the Kalman filtering is represented. Application of this algorithm allows to improve the accuracy of the aircraft motion parameter estimation. For an optical horizon sensor a self-contained horizon recognition algorithm that enables real-time aircraft attitude determination relative to the horizon line is developed. A scaled-down simulation and performance analysis of the operation of the integrated navigation system is carried out.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"20 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126406958","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":"Convergence properties of an online learning algorithm in neural network models of complex systems","authors":"V. Azarskov, S. Nikolaienko, L. Zhiteckii","doi":"10.1109/APUAVD.2013.6705293","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705293","url":null,"abstract":"Asymptotic behavior of the online gradient algorithm with a constant step size employed for learning in neural network models of nonlinear systems having hidden layer are studied. The sufficient conditions guaranteeing the convergence of this algorithm in the random environment are established.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"221 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116375818","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":"Phase Doppler signal filtering in two-wave laser Doppler anemometer","authors":"V. Zemlyanskiy, M. Gusev, A. P. Chudesov","doi":"10.1109/APUAVD.2013.6705292","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705292","url":null,"abstract":"Onboard equipment of unmanned aerial vehicle (UAV) should be small-sized and have a minimum possible weight. This rigid requirement also applies to the onboard laser velocimetry (anemometer, laser Doppler anemometer (LDA)) which can be realized not only on the base of integral optics using, semiconductor lasers and nanotechnologies in the production of element base of LDA, but also on the base of new physical and technological solutions during the construction of LDA's principal scheme. Simultaneous using of the phase-coherent spatial filtration of signals at different wavelengths, conditions' fulfillment of optimal receiving provides achievement of relation signal/noise on the output of two-wave LDA at least at one order in comparison of known LDA's schemes. It gives a possibility for significantly increasing of velocity measurement's accuracy with the help of two-wave LDA's new generation.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"10 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128801947","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":"Performance parameters comparison of ring laser, coriolis vibratory and fiber-optic gyros based on Allan variance analysis","authors":"V. Chikovani","doi":"10.1109/APUAVD.2013.6705312","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705312","url":null,"abstract":"On the basis of Allan variance analysis performance parameters of ring laser, Coriolis vibratory and fiber optic gyros comparison is conducted. Manufacturers of the analyzed gyros are from USA, Russia and Ukraine. The main reason of this work is to determine potential performance of the developed in Ukraine low-cost metallic cylindrical resonator Coriolis vibratory gyro in comparison to high accuracy ring laser gyro produced by well-known USA company Honeywell and middle accuracy fiber optic gyro produced by Russian company Fizoptica.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"92 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116666413","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":"Integration of unified modules of aircraft onboard navigation and landing equipment for \"small aviation\"","authors":"A. Osipchuk","doi":"10.1109/APUAVD.2013.6705298","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705298","url":null,"abstract":"The possibility of integration of unified modules onboard navigation and landing equipment is defined. The different variants of the unified units depending on the destination are known. The brief comparative analysis is made.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"9 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127704128","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 filtering of temperature errors for coriolis vibratory gyroscopes","authors":"V. Apostolyuk","doi":"10.1109/APUAVD.2013.6705295","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705295","url":null,"abstract":"Optimal static filter of stochastic temperature disturbances is proposed in this paper. Filter is based on the model of the temperature variations influences via undesired cross-damping. Instead of temperature measurements its power spectral density is used along with the corresponding model of the moving object dynamics.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"37 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121287530","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":"Providing guaranteed accuracy of control at arbitrary disturbances","authors":"O. Kopysov","doi":"10.1109/APUAVD.2013.6705299","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705299","url":null,"abstract":"An adaptive algorithm for one class of control systems with guaranteed accuracy at arbitrary disturbances is proposed. Such problem does not have a clear solution for today. Known robust methods provide good properties of the system only in a certain range of disturbances or changes in steady-state modes of operation and a priori information about the disturbance. Also they implement forecasting of control system dynamics without evaluation of existing disturbances. Regulators in such control systems generally have high dimensionality, and sometimes they should have essentially nonlinear properties. The issues of low-order controllers designing with quite simple construction, which provide the desired control accuracy for arbitrary disturbances and in non-stationary modes, require further development. The proposed algorithm is based on an indirect estimation of the resulting effects and predicting of the control object controlled variable, by means of which current value of the feedback coefficient is obtained, such that the controlled variable does not exceed the permissible value.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"67 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115945849","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":"The generalized classification of Unmanned Air Vehicles","authors":"A. Korchenko, O. Illyash","doi":"10.1109/APUAVD.2013.6705275","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705275","url":null,"abstract":"According to a generalization of common classifications and performance characteristics of existing Unmanned Air Vehicles, this article calls attention to its classification which is based on 16 the fundamental features: 1) aircraft applications; 2) type of a control system; 3) flight rules; 4) airspace classification; 5) aircraft types; 6) wing types; 7) takeoff/landing direction; 8) types of take-off/landing; 9) aircraft engine types; 10) fuel system; 11) fuel tank types; 12) number of exploitations; 13) category (according to the weight and maximum range of flight UAV); 14) flight radius; 15) flight altitude; 16) Aircraft Functions.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125345025","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}