Pub Date : 2017-10-01DOI: 10.1109/APUAVD.2017.8308805
H. M. Guzey
Neural Network-based adaptive consensus control is designed in this paper for a team of fixed-wing unmanned aerial vehicles. The group of unmanned aerial vehicles moving at fixed altitudes are controlled through a novel adaptive formation controller to drive them to a pre-defined formation shape. The theoretical conjecture is verified by simulation results.
{"title":"Adaptive consensus-based formation control of fixed-wing MUAV's","authors":"H. M. Guzey","doi":"10.1109/APUAVD.2017.8308805","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308805","url":null,"abstract":"Neural Network-based adaptive consensus control is designed in this paper for a team of fixed-wing unmanned aerial vehicles. The group of unmanned aerial vehicles moving at fixed altitudes are controlled through a novel adaptive formation controller to drive them to a pre-defined formation shape. The theoretical conjecture is verified by simulation results.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"282 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116563465","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308765
V. Sineglazov, V. S. Ischenko
Unmanned aerial vehicle flight simulation bench for visual navigation system. Visual navigation system gives opportunity to flight in radio interference zone. Considered approach for adjustment and evaluating visual navigation system.
{"title":"Visual navigation system adjustment","authors":"V. Sineglazov, V. S. Ischenko","doi":"10.1109/APUAVD.2017.8308765","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308765","url":null,"abstract":"Unmanned aerial vehicle flight simulation bench for visual navigation system. Visual navigation system gives opportunity to flight in radio interference zone. Considered approach for adjustment and evaluating visual navigation system.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"66 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130671055","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308799
R. Odarchenko, Oleh Polihenko, L. Kharlai, O. Tkalich
Was proposed improved method for estimation of the communication range and bandwidth of unmanned aerial vehicle communication systems in the complex conditions of multibeam radio waves propagation with the help of Multiple-Input-Multiple-Output systems. The model of determining effective bandwidth, which is based on using both subchannels using various modulation schemes in the Multiple-Input-Multiple-Output systems channels. The results of calculations and simulations confirm the high efficiency of the method.
{"title":"Estimation of the communication range and bandwidth of UAV communication systems","authors":"R. Odarchenko, Oleh Polihenko, L. Kharlai, O. Tkalich","doi":"10.1109/APUAVD.2017.8308799","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308799","url":null,"abstract":"Was proposed improved method for estimation of the communication range and bandwidth of unmanned aerial vehicle communication systems in the complex conditions of multibeam radio waves propagation with the help of Multiple-Input-Multiple-Output systems. The model of determining effective bandwidth, which is based on using both subchannels using various modulation schemes in the Multiple-Input-Multiple-Output systems channels. The results of calculations and simulations confirm the high efficiency of the method.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132766340","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308789
V. Kharchenko, N. Kuzmenko, I. Ostroumov
The problem of unmanned aerial vehicle flight situation identification was considered. Classification of flight situation includes five classes according to the degree of danger. The classification is based on the value of parameters deviation from planed values. Proposed approach takes into account different types of unmanned aerial vehicles that makes it universal for each flight task. As a result, identification of the current flight situation increases situation awareness of a pilot and insures the required level of flight safety.
{"title":"Identification of unmanned aerial vehicle flight situation","authors":"V. Kharchenko, N. Kuzmenko, I. Ostroumov","doi":"10.1109/APUAVD.2017.8308789","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308789","url":null,"abstract":"The problem of unmanned aerial vehicle flight situation identification was considered. Classification of flight situation includes five classes according to the degree of danger. The classification is based on the value of parameters deviation from planed values. Proposed approach takes into account different types of unmanned aerial vehicles that makes it universal for each flight task. As a result, identification of the current flight situation increases situation awareness of a pilot and insures the required level of flight safety.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"86 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133390961","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308781
O. Kutsenko, S. Ilnytska, V. Kondratyuk, V. Konin
Due to significant potential benefits provided by unmanned aerial vehicles, their usage continues to grow in different application spheres. Development of reliable unmanned aerial vehicle navigation and control systems, and landing system, in particular, conclude very complex and interesting task, with which engineers and designers face. This paper presents the method of unmanned aerial vehicle position determination in Global Navigation Satellite System landing system for the cases when precise coordinates of reference receiver and runway are unknown and when they are known in advance. It has been experimentally proved the correctness of the presented method for the case when unmanned aerial vehicle is landing at the airdrome with precisely defined Final Approach Segment data block parameters.
{"title":"Unmanned aerial vehicle position determination in GNSS landing system","authors":"O. Kutsenko, S. Ilnytska, V. Kondratyuk, V. Konin","doi":"10.1109/APUAVD.2017.8308781","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308781","url":null,"abstract":"Due to significant potential benefits provided by unmanned aerial vehicles, their usage continues to grow in different application spheres. Development of reliable unmanned aerial vehicle navigation and control systems, and landing system, in particular, conclude very complex and interesting task, with which engineers and designers face. This paper presents the method of unmanned aerial vehicle position determination in Global Navigation Satellite System landing system for the cases when precise coordinates of reference receiver and runway are unknown and when they are known in advance. It has been experimentally proved the correctness of the presented method for the case when unmanned aerial vehicle is landing at the airdrome with precisely defined Final Approach Segment data block parameters.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128549744","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308783
A. Ablesimov, M. Pylypenko, A. M. Ryabokonev, K. Adamchuk
Analyzed the properties of corrective devices for remotely controlled aerial vehicles and are designed algorithms for calculating their frequency characteristics.
分析了遥控飞行器校正装置的特性，设计了校正装置频率特性的计算算法。
{"title":"Correction of quality of control systems of remotely controlled aerial vehicles","authors":"A. Ablesimov, M. Pylypenko, A. M. Ryabokonev, K. Adamchuk","doi":"10.1109/APUAVD.2017.8308783","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308783","url":null,"abstract":"Analyzed the properties of corrective devices for remotely controlled aerial vehicles and are designed algorithms for calculating their frequency characteristics.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"31 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132753606","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308813
S. Pavlova, V. Chepizhenko
A methodology has been proposed that is aimed at the development and improvement of modern methods, models and algorithms for synergetic intelligent control of unmanned aerial vehicle formations.
提出了一种方法，旨在发展和改进用于无人机编队协同智能控制的现代方法、模型和算法。
{"title":"The methodology of synthesis of synergetic intelligent control of UAV formations","authors":"S. Pavlova, V. Chepizhenko","doi":"10.1109/APUAVD.2017.8308813","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308813","url":null,"abstract":"A methodology has been proposed that is aimed at the development and improvement of modern methods, models and algorithms for synergetic intelligent control of unmanned aerial vehicle formations.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"182 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121711013","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308777
V. Sineglazov, A. Godny
Presented navigation system for unmanned aerial vehicles based on microservices with an integrated environment introduces a new approach to managing the design process. Used in the proposed medium design scenario can greatly simplify the work of the designer. Available in medium monitor provides the flexibility of design processes with a flexible structure description of design procedures in the design scenario.
{"title":"Dynamic aided-design of UAV navigation systems","authors":"V. Sineglazov, A. Godny","doi":"10.1109/APUAVD.2017.8308777","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308777","url":null,"abstract":"Presented navigation system for unmanned aerial vehicles based on microservices with an integrated environment introduces a new approach to managing the design process. Used in the proposed medium design scenario can greatly simplify the work of the designer. Available in medium monitor provides the flexibility of design processes with a flexible structure description of design procedures in the design scenario.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"16 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117133903","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308821
V. Sherstjuk, M. Zharikova, Igor Sokol
This work presents the soft topology model and the method of finding the suitable compensation for vehicles' activity scenarios that can keeping spatial configuration and satisfying safety restrictions for the vehicle onboard control system. The qualitative safety assessment is proposed, the implementation of the method based on the soft level topology is presented. The proposed method has acceptable computational complexity.
{"title":"Maintaining the order of heterogeneous ensemble of unmanned vehicles using level soft topology","authors":"V. Sherstjuk, M. Zharikova, Igor Sokol","doi":"10.1109/APUAVD.2017.8308821","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308821","url":null,"abstract":"This work presents the soft topology model and the method of finding the suitable compensation for vehicles' activity scenarios that can keeping spatial configuration and satisfying safety restrictions for the vehicle onboard control system. The qualitative safety assessment is proposed, the implementation of the method based on the soft level topology is presented. The proposed method has acceptable computational complexity.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"362 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115900918","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 : 2017-10-01DOI: 10.1109/APUAVD.2017.8308793
V. Avrutov, D. Buhaiov, V. Meleshko
A gyrocompassing mode of the attitude heading reference system was presented. Attitude heading reference system has been composed of inertial measurement unit and navigation computer. Inertial measurement unit consists of triad accelerometers, gyroscopes and a circuit of signal processing. It is received a full expression for the error of gyrocompassing depending from errors of gyroscope, accelerometers and latitude source. It was estimated the errors of gyroscope and accelerometers on the assumption of the required the error of gyrocompassing. Also, it is shown that calibration results are effected to the error of gyrocompassing. It is brought the simulation results of impact any factors such as bias instability of gyroscopes, scale factor instability of gyroscopes, bias instability of accelerometers, scale factor instability of accelerometers, and misalignment of measurement frame axes onto the error of gyrocompassing mode. It is shown that maximum influence on to the error of gyrocom-passing mode has got the bias instability of gyroscopes.
{"title":"Gyrocompassing mode of the attitude and heading reference system","authors":"V. Avrutov, D. Buhaiov, V. Meleshko","doi":"10.1109/APUAVD.2017.8308793","DOIUrl":"https://doi.org/10.1109/APUAVD.2017.8308793","url":null,"abstract":"A gyrocompassing mode of the attitude heading reference system was presented. Attitude heading reference system has been composed of inertial measurement unit and navigation computer. Inertial measurement unit consists of triad accelerometers, gyroscopes and a circuit of signal processing. It is received a full expression for the error of gyrocompassing depending from errors of gyroscope, accelerometers and latitude source. It was estimated the errors of gyroscope and accelerometers on the assumption of the required the error of gyrocompassing. Also, it is shown that calibration results are effected to the error of gyrocompassing. It is brought the simulation results of impact any factors such as bias instability of gyroscopes, scale factor instability of gyroscopes, bias instability of accelerometers, scale factor instability of accelerometers, and misalignment of measurement frame axes onto the error of gyrocompassing mode. It is shown that maximum influence on to the error of gyrocom-passing mode has got the bias instability of gyroscopes.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128746596","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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