Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705305
V. Sineglazov, Yurii Shmelev
Qualification level control of remotely piloted aircraft pilots is considered. The approach of informational resources distribution is proposed. It is based on application of theory of information.
考虑了遥控飞机驾驶员的资格水平控制。提出了信息资源分配的方法。它是基于信息论的应用。
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Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705326
O. Ablesimov, A. Gonchar
The principles of the automatic control systems realization when a priori information about external disturbances acting on plants is incomplete are considered.
研究了当外界干扰的先验信息不完全时自动控制系统的实现原理。
{"title":"Adaptive control system for UAV with state observer","authors":"O. Ablesimov, A. Gonchar","doi":"10.1109/APUAVD.2013.6705326","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705326","url":null,"abstract":"The principles of the automatic control systems realization when a priori information about external disturbances acting on plants is incomplete are considered.","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":"122937204","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}
Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705276
D. Shevchuk
Safety of aircraft during the flight is one of the most important problems that concerns of all aviation. Damage to the external contour of the aircraft by foreign objects always leads to a change in the characteristics of the aircraft, direct and indirect economic costs and sometimes to injury or death of passengers and crew. Real-time external contour diagnostics of the aircraft and wings makes it possible to warn or prevent emergency situations and thus improve safety. The modeling of such effects is necessary for the development of reconfiguration flight control systems to recover aircraft controllability from adverse, damage-related loss-of-control events, as well as for the estimation of aerodynamic characteristics from extra conditions in flight.
{"title":"Diagnostics of aircraft aerodynamics changes in emergency situation in flight","authors":"D. Shevchuk","doi":"10.1109/APUAVD.2013.6705276","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705276","url":null,"abstract":"Safety of aircraft during the flight is one of the most important problems that concerns of all aviation. Damage to the external contour of the aircraft by foreign objects always leads to a change in the characteristics of the aircraft, direct and indirect economic costs and sometimes to injury or death of passengers and crew. Real-time external contour diagnostics of the aircraft and wings makes it possible to warn or prevent emergency situations and thus improve safety. The modeling of such effects is necessary for the development of reconfiguration flight control systems to recover aircraft controllability from adverse, damage-related loss-of-control events, as well as for the estimation of aerodynamic characteristics from extra conditions in flight.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"111 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":"114751278","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}
Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705325
V. M. Konyushko
The paper deals with analysis of unmanned aerial vehicles control systems. The characteristics of modern UAVs are close to those of modern aircraft and the main components of UAVs control systems will use the same devices of modern aircraft. The main emphasis is made on the usage of modern microcontrollers and FPGAs (field programmable gate arrays).
{"title":"Features of UAV control systems assessing","authors":"V. M. Konyushko","doi":"10.1109/APUAVD.2013.6705325","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705325","url":null,"abstract":"The paper deals with analysis of unmanned aerial vehicles control systems. The characteristics of modern UAVs are close to those of modern aircraft and the main components of UAVs control systems will use the same devices of modern aircraft. The main emphasis is made on the usage of modern microcontrollers and FPGAs (field programmable gate arrays).","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"32 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":"125804318","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}
Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705324
V. I. Kashmatov
The paper deals with the principle of construction of the three-axes kinesthetic panel for the quasi-object control by the angular position of unmanned aerial vehicle. The principle of operation of the represented panel and the used systems of coordinates are represented. The possible area of the suggested panel is described.
{"title":"Kinesthetic panel for quasi-object control by UAV","authors":"V. I. Kashmatov","doi":"10.1109/APUAVD.2013.6705324","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705324","url":null,"abstract":"The paper deals with the principle of construction of the three-axes kinesthetic panel for the quasi-object control by the angular position of unmanned aerial vehicle. The principle of operation of the represented panel and the used systems of coordinates are represented. The possible area of the suggested panel is described.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"80 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":"116091376","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}
Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705318
O. Sushchenko, A. Tunik
This paper deals with the problems of stabilization of the observation equipment operated at the unmanned aerial vehicles in difficult conditions of the vigorous disturbances. The mathematical model of the triaxial stabilization system is developed. The problem statement and basic stages of the robust structural synthesis are analyzed. The results of the synthesized system simulation are given.
{"title":"Robust stabilization of UAV observation equipment","authors":"O. Sushchenko, A. Tunik","doi":"10.1109/APUAVD.2013.6705318","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705318","url":null,"abstract":"This paper deals with the problems of stabilization of the observation equipment operated at the unmanned aerial vehicles in difficult conditions of the vigorous disturbances. The mathematical model of the triaxial stabilization system is developed. The problem statement and basic stages of the robust structural synthesis are analyzed. The results of the synthesized system simulation are given.","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":"130132671","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}
Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705302
E. Abramov, A. V. Abramova, D. Konotop
The paper describes the process of complex technical object design on the example of the aircraft, using information technology such as CAD/CAM/CAE-systems. The paper discloses a weight design process, which is associated with all stages of aircraft development and its production. Knowledge-oriented approach of the CTO design gives the possibility of managing geometrical and weight model parameters on all stages of the CTO design. Such structure of automatized CTO design system allows taking into account classic and innovative methods of CTO design, combining them in accordance with their exactness at the calculation composition of CTO parameters.
{"title":"Knowledge — Oriented support of complex technical object design","authors":"E. Abramov, A. V. Abramova, D. Konotop","doi":"10.1109/APUAVD.2013.6705302","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705302","url":null,"abstract":"The paper describes the process of complex technical object design on the example of the aircraft, using information technology such as CAD/CAM/CAE-systems. The paper discloses a weight design process, which is associated with all stages of aircraft development and its production. Knowledge-oriented approach of the CTO design gives the possibility of managing geometrical and weight model parameters on all stages of the CTO design. Such structure of automatized CTO design system allows taking into account classic and innovative methods of CTO design, combining them in accordance with their exactness at the calculation composition of CTO parameters.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"58 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":"124666393","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}
Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705315
T. A. Galaguz
In the paper the structural - parametric synthesis of UAV flight control systems is carried out. To restore the state vector, which contains incomplete measurements with noise, the Kalman filter or Luenberger observer are included into the control law. Based on the received results the comparative analysis of the control systems efficiency is performed.
{"title":"Comparison of UAV control systems designed by means of Kalman filter and Luenberger observer","authors":"T. A. Galaguz","doi":"10.1109/APUAVD.2013.6705315","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705315","url":null,"abstract":"In the paper the structural - parametric synthesis of UAV flight control systems is carried out. To restore the state vector, which contains incomplete measurements with noise, the Kalman filter or Luenberger observer are included into the control law. Based on the received results the comparative analysis of the control systems efficiency is performed.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"119 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":"124325283","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}
Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705279
V. Sineglazov, S. I. Askerov
The design procedure of unmanned aerial vehicle navigation complexes with given characteristics is considered. The structure of integrated navigation complex is determined.
考虑了具有给定特性的无人机导航综合体的设计过程。确定了综合导航综合体的结构。
{"title":"Computer aided design of UAV navigation complexes with given characteristics","authors":"V. Sineglazov, S. I. Askerov","doi":"10.1109/APUAVD.2013.6705279","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705279","url":null,"abstract":"The design procedure of unmanned aerial vehicle navigation complexes with given characteristics is considered. The structure of integrated navigation complex is determined.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"16 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":"123678681","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}
Pub Date : 2013-10-01DOI: 10.1109/APUAVD.2013.6705288
O. Solomentsev, M. Zaliskyi, O. Zuiev, M. Asanov
An application of sequential procedures for parameters statistical estimation in engineering practice is described. As an example the process of monitoring the reliability of unmanned vehicles radioelectronic equipment is taken. A comparative analysis of three variants of data processing structures in exploitation systems is made.
{"title":"Data processing in exploitation system of unmanned aerial vehicles radioelectronic equipment","authors":"O. Solomentsev, M. Zaliskyi, O. Zuiev, M. Asanov","doi":"10.1109/APUAVD.2013.6705288","DOIUrl":"https://doi.org/10.1109/APUAVD.2013.6705288","url":null,"abstract":"An application of sequential procedures for parameters statistical estimation in engineering practice is described. As an example the process of monitoring the reliability of unmanned vehicles radioelectronic equipment is taken. A comparative analysis of three variants of data processing structures in exploitation systems is made.","PeriodicalId":400843,"journal":{"name":"2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)","volume":"15 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":"117334010","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}
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