Pub Date : 2017-05-01DOI: 10.1109/ICMSC.2017.7959503
A. Kostoglotov, Igor Deryabkin, D. Andrashitov, S. Lazarenko, A. Kuznetcov
The use of the combined maximum principle provides a constructive solution to the problem of tracking the maneuvering aircraft in the form of the inverse dynamics problem. In the article based on this approach the effective tracking filter is developed. It is based on the combined use of techniques for construction the synthesis function and the approach, which consists in considering the unknown forces to be determined, as a mixture of disturbing and control actions. The efficiency is understood in the sense of high precision and stability of the estimation algorithms, and a comparatively small computational complexity.
{"title":"Method of estimation algorithms synthesis of dynamic processes with construction of the reference trajectory in transients disturbances","authors":"A. Kostoglotov, Igor Deryabkin, D. Andrashitov, S. Lazarenko, A. Kuznetcov","doi":"10.1109/ICMSC.2017.7959503","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959503","url":null,"abstract":"The use of the combined maximum principle provides a constructive solution to the problem of tracking the maneuvering aircraft in the form of the inverse dynamics problem. In the article based on this approach the effective tracking filter is developed. It is based on the combined use of techniques for construction the synthesis function and the approach, which consists in considering the unknown forces to be determined, as a mixture of disturbing and control actions. The efficiency is understood in the sense of high precision and stability of the estimation algorithms, and a comparatively small computational complexity.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"60 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132535617","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 : 2017-05-01DOI: 10.1109/ICMSC.2017.7959498
A. Maffei, M. Onori, M. R. Khabbazi, J. Wikander, Ellen Bergseth
This paper introduces the assembly feature data schema instance modeling to pre-examine the schema functionality and output-as the preliminary step for data modeling. In order to link assembly with product design, it is essential to determine which entities of product design are involved at the automated assembly planning and operations. It is possible to assign meaningful attributes (assembly features) to the part model entities in a systematic and structured way. Using object-oriented design, the assembly feature data structure and its relationships are modeled. As a part of the research on product and assembly system data integration within the evolvable production system platform, the instance models for proposed assembly feature data structure provide a deeper understanding and error reduction that might possibly occur at the development of the database. Moreover through instance modeling, the assembly feature data query output format from the database prototype is simulated. An industrial assembly model example with its 3DPart models is chosen to demonstrate the realized assembly feature data set with string data type. The models support the desired simplicity at the database prototype implementation. The output format envisions the interoperability factor between product models and the assembly planning systems.
{"title":"Assembly feature data instance modeling: Prototype implementation and outputs","authors":"A. Maffei, M. Onori, M. R. Khabbazi, J. Wikander, Ellen Bergseth","doi":"10.1109/ICMSC.2017.7959498","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959498","url":null,"abstract":"This paper introduces the assembly feature data schema instance modeling to pre-examine the schema functionality and output-as the preliminary step for data modeling. In order to link assembly with product design, it is essential to determine which entities of product design are involved at the automated assembly planning and operations. It is possible to assign meaningful attributes (assembly features) to the part model entities in a systematic and structured way. Using object-oriented design, the assembly feature data structure and its relationships are modeled. As a part of the research on product and assembly system data integration within the evolvable production system platform, the instance models for proposed assembly feature data structure provide a deeper understanding and error reduction that might possibly occur at the development of the database. Moreover through instance modeling, the assembly feature data query output format from the database prototype is simulated. An industrial assembly model example with its 3DPart models is chosen to demonstrate the realized assembly feature data set with string data type. The models support the desired simplicity at the database prototype implementation. The output format envisions the interoperability factor between product models and the assembly planning systems.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"105 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116420131","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 : 2017-05-01DOI: 10.5815/IJISA.2017.06.01
N. Karabutov
The method of construction adaptive observers (AO) time-varying linear dynamic objects at non-fulfillment of a condition an excitation constancy (EC) is proposed. Synthesis of the adaptive observer is given as the solution of two tasks. The solution first a problem is a choice of the constant matrix decreasing the effect of EC condition. The solution of the second problem gives a method of synthesis adaptive multiplicative algorithms in the presence of the obtained restrictions. Procedures of an estimation uncertainty in an object are proposed.
{"title":"Adaptive observers for linear time-varying dynamic objects","authors":"N. Karabutov","doi":"10.5815/IJISA.2017.06.01","DOIUrl":"https://doi.org/10.5815/IJISA.2017.06.01","url":null,"abstract":"The method of construction adaptive observers (AO) time-varying linear dynamic objects at non-fulfillment of a condition an excitation constancy (EC) is proposed. Synthesis of the adaptive observer is given as the solution of two tasks. The solution first a problem is a choice of the constant matrix decreasing the effect of EC condition. The solution of the second problem gives a method of synthesis adaptive multiplicative algorithms in the presence of the obtained restrictions. Procedures of an estimation uncertainty in an object are proposed.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"106 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114272649","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 : 2017-05-01DOI: 10.1109/ICMSC.2017.7959508
M. Salimi, M. Hamedi
Modern control approaches are completely studied in standard DC-DC buck and boost converters. However, industrial switching power supplies haven't been investigated precisely using nonlinear control systems. This issue is related to more complex state-space model of these converters. In this paper, adaptive nonlinear control of isolated flyback switching power supplies is studied using Lyapunov stability analysis. In spite of large variations in load and line, proposed closed-loop system is able to stabilize and regulate output state variable of the flyback converter in different operational conditions without steady-state error. Considering presence of Right Half Plan Zero (RHPZ) in transfer function of the isolated flyback switching power supply, proposed controller employs the double-loop cascaded structure which includes a separate voltage loop to improve steady-state and dynamic responses. Estimated values of the system uncertain parameters are employed for implementation of the controller and hence fast dynamic response can be obtained during system startup and parameters changes. Finally designed isolated flyback chopper is simulated in MATLAB/Simulink in different operating points to investigate accuracy of the proposed controller.
{"title":"Adaptive nonlinear control of the flyback switch mode power supplies","authors":"M. Salimi, M. Hamedi","doi":"10.1109/ICMSC.2017.7959508","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959508","url":null,"abstract":"Modern control approaches are completely studied in standard DC-DC buck and boost converters. However, industrial switching power supplies haven't been investigated precisely using nonlinear control systems. This issue is related to more complex state-space model of these converters. In this paper, adaptive nonlinear control of isolated flyback switching power supplies is studied using Lyapunov stability analysis. In spite of large variations in load and line, proposed closed-loop system is able to stabilize and regulate output state variable of the flyback converter in different operational conditions without steady-state error. Considering presence of Right Half Plan Zero (RHPZ) in transfer function of the isolated flyback switching power supply, proposed controller employs the double-loop cascaded structure which includes a separate voltage loop to improve steady-state and dynamic responses. Estimated values of the system uncertain parameters are employed for implementation of the controller and hence fast dynamic response can be obtained during system startup and parameters changes. Finally designed isolated flyback chopper is simulated in MATLAB/Simulink in different operating points to investigate accuracy of the proposed controller.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"63 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123829440","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 : 2017-05-01DOI: 10.1109/ICMSC.2017.7959435
L. Belyaev, A. Zhdanov, V. Morozov
The use of the implantable left ventricle assist device (LVAD) and total artificial heart (TAH) systems is one of the most widespread methods of heart failure treatment. In Russia, the pulsative type systems have got the biggest distribution in clinical practice. During the design of the specified systems complex technical challenges were solved, some of them were the selection of the materials and the manufacturing technologies of artificial heart ventricle. The objective of this article is the description of the applied materials to produce artificial heart ventricles of the Russian pulsative type LVAD and TAH systems, also the review and the critical analysis of possible technologies for their production. Based on the analysis of features of manufacturing technologies and medical-technical requirements to an artificial heart ventricle, manufacturing technologies of components of artificial heart ventricle from the Russian material "Vitur" are proposed. The stage of technological preparation of production is realized with application of CADCAMCAE-systems. The design results of industrial equipment for production of an artificial heart ventricle and the samples of the obtained products, which have been successfully tested under laboratory-bench conditions as part of the pulsative type LVAD and TAH systems with a pneumatic and electromechanical drive, are presented.
{"title":"Materials and technologies for pulsative Russian artificial heart ventricle manufacturing","authors":"L. Belyaev, A. Zhdanov, V. Morozov","doi":"10.1109/ICMSC.2017.7959435","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959435","url":null,"abstract":"The use of the implantable left ventricle assist device (LVAD) and total artificial heart (TAH) systems is one of the most widespread methods of heart failure treatment. In Russia, the pulsative type systems have got the biggest distribution in clinical practice. During the design of the specified systems complex technical challenges were solved, some of them were the selection of the materials and the manufacturing technologies of artificial heart ventricle. The objective of this article is the description of the applied materials to produce artificial heart ventricles of the Russian pulsative type LVAD and TAH systems, also the review and the critical analysis of possible technologies for their production. Based on the analysis of features of manufacturing technologies and medical-technical requirements to an artificial heart ventricle, manufacturing technologies of components of artificial heart ventricle from the Russian material \"Vitur\" are proposed. The stage of technological preparation of production is realized with application of CADCAMCAE-systems. The design results of industrial equipment for production of an artificial heart ventricle and the samples of the obtained products, which have been successfully tested under laboratory-bench conditions as part of the pulsative type LVAD and TAH systems with a pneumatic and electromechanical drive, are presented.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131385166","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 : 2017-05-01DOI: 10.1109/ICMSC.2017.7959449
Zhaohui Wang, Si Chen, Xiaogang Deng
Based on the mechanism of the cavitation effect in the self-excited oscillation pulsed jet nozzle, a modified cavitation model is proposed for improving the precision of the simulation, which considers the influence of Reynolds shear stress, the viscous shear stress and the turbulent pressure fluctuations existed in the shear layer on the vapor pressure. The modified cavitation model is hooked in the Fluent through the user defined function (UDF) to define the vapor pressure property which plays a role of criterion for cavitation. The fluctuation, frequency and magnitude distribution of the velocity at the outlet of the nozzle are analyzed and compared with the corresponding results obtained by using the original cavitation model. It is observed that the results obtained by the modified model are more consistent with the actual working situation of the nozzle. Finally, the effect of the inlet pressure on the occurrence of the cavitaion is investigated for exploring the relationship of the cavitation chance and the factors considered in the modified cavitation.
{"title":"Research on modified cavitation model for self-excited oscillation pulsed jet nozzle","authors":"Zhaohui Wang, Si Chen, Xiaogang Deng","doi":"10.1109/ICMSC.2017.7959449","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959449","url":null,"abstract":"Based on the mechanism of the cavitation effect in the self-excited oscillation pulsed jet nozzle, a modified cavitation model is proposed for improving the precision of the simulation, which considers the influence of Reynolds shear stress, the viscous shear stress and the turbulent pressure fluctuations existed in the shear layer on the vapor pressure. The modified cavitation model is hooked in the Fluent through the user defined function (UDF) to define the vapor pressure property which plays a role of criterion for cavitation. The fluctuation, frequency and magnitude distribution of the velocity at the outlet of the nozzle are analyzed and compared with the corresponding results obtained by using the original cavitation model. It is observed that the results obtained by the modified model are more consistent with the actual working situation of the nozzle. Finally, the effect of the inlet pressure on the occurrence of the cavitaion is investigated for exploring the relationship of the cavitation chance and the factors considered in the modified cavitation.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"9 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115081369","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 : 2017-05-01DOI: 10.1109/ICMSC.2017.7959459
M. Aydin, Ramazan Coban
In this study, first-order and second-order sliding mode speed controller for the Precision Modular Servo (PMS) setup produced by Feedback Instruments is proposed. The second-order sliding mode controller which permits decimate of the chattering phenomena is designed to control the real time speed of this electromechanical system. The Lyapunov stability theorem is used to confirm the stability of the system. And first-order and second-order sliding mode speed controllers are compared with each other. Experimental results are compared under condition of the same control strategy. The experimental results confirm that the offered super-twisting algorithm sliding mode controller eliminates the chattering while preserving the robustness of the control.
{"title":"Second-order sliding mode control design and experimental application to a servo motor","authors":"M. Aydin, Ramazan Coban","doi":"10.1109/ICMSC.2017.7959459","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959459","url":null,"abstract":"In this study, first-order and second-order sliding mode speed controller for the Precision Modular Servo (PMS) setup produced by Feedback Instruments is proposed. The second-order sliding mode controller which permits decimate of the chattering phenomena is designed to control the real time speed of this electromechanical system. The Lyapunov stability theorem is used to confirm the stability of the system. And first-order and second-order sliding mode speed controllers are compared with each other. Experimental results are compared under condition of the same control strategy. The experimental results confirm that the offered super-twisting algorithm sliding mode controller eliminates the chattering while preserving the robustness of the control.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"59 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129682438","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 : 2017-05-01DOI: 10.1109/ICMSC.2017.7959456
V. Kuz'michev, A. Tkachenko, E. P. Filinov, I. Krupenich, Yaroslav A. Ostapyuk
This article describes the results of optimization of the working process parameters (overall pressure ratio and turbine inlet temperature) of small-scale turbojet for cruise missiles and target airplanes. The influence of engine scale factor upon the efficiency of turbomachines, as well as the principal operational constraints were taken into account during the multi-criteria optimization. Specific fuel consumption and the total mass of engine and required fuel were selected as the optimization criteria. Optimal regions of the working process parameters were identified for the turbojet engines of thrust ranging from 0.1 kN to 2 kN. The results show that different types of turbomachinery (e.g. axial vs. centrifugal compressor) have substantially different optimal regions, thus the stage of optimization of working process parameters for the small-scale engines could not be implemented independently, unlike the full-sized engines. According to results, the optimal values of working process parameters decrease as the engine scale factor decreases, and the optimal regions shrink too. The results presented in this paper also include the most efficient values of the working process parameters and the rational types of turbomachines for various thrust levels and aircraft missions.
{"title":"Optimization of working process parameters of small-scale turbojet for unmanned aircraft","authors":"V. Kuz'michev, A. Tkachenko, E. P. Filinov, I. Krupenich, Yaroslav A. Ostapyuk","doi":"10.1109/ICMSC.2017.7959456","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959456","url":null,"abstract":"This article describes the results of optimization of the working process parameters (overall pressure ratio and turbine inlet temperature) of small-scale turbojet for cruise missiles and target airplanes. The influence of engine scale factor upon the efficiency of turbomachines, as well as the principal operational constraints were taken into account during the multi-criteria optimization. Specific fuel consumption and the total mass of engine and required fuel were selected as the optimization criteria. Optimal regions of the working process parameters were identified for the turbojet engines of thrust ranging from 0.1 kN to 2 kN. The results show that different types of turbomachinery (e.g. axial vs. centrifugal compressor) have substantially different optimal regions, thus the stage of optimization of working process parameters for the small-scale engines could not be implemented independently, unlike the full-sized engines. According to results, the optimal values of working process parameters decrease as the engine scale factor decreases, and the optimal regions shrink too. The results presented in this paper also include the most efficient values of the working process parameters and the rational types of turbomachines for various thrust levels and aircraft missions.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125697211","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 : 2017-05-01DOI: 10.1109/ICMSC.2017.7959488
D. Phaoharuhansa
This paper investigates on a development of free floating point absorber type of ocean wave energy converter (OWEC) for the gulf of Thailand. The point absorber is designed based on a double mass-spring system. The electric generators are installed in the buoy body and they will slide on a column as harmonic motion. The point absorber is demonstrated in open water channel with wave input. The amplitude and the frequency of the wave are varied, and then the electric power output and the motion of the generators are measured during the wave input. The experiment result presents the relationship between the electricity and stiffness of springs. The peak power output is 1,185 mW that the wave's amplitude is 0.05 m, the frequency is 2 Π rad/s, and the stiffness of the spring is 285 N.m. Thus, the peak power output is approximately 14,000 mW for wave's amplitude and wave's frequency in the gulf of Thailand.
{"title":"Development of ocean wave energy converter for gulf of Thailand","authors":"D. Phaoharuhansa","doi":"10.1109/ICMSC.2017.7959488","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959488","url":null,"abstract":"This paper investigates on a development of free floating point absorber type of ocean wave energy converter (OWEC) for the gulf of Thailand. The point absorber is designed based on a double mass-spring system. The electric generators are installed in the buoy body and they will slide on a column as harmonic motion. The point absorber is demonstrated in open water channel with wave input. The amplitude and the frequency of the wave are varied, and then the electric power output and the motion of the generators are measured during the wave input. The experiment result presents the relationship between the electricity and stiffness of springs. The peak power output is 1,185 mW that the wave's amplitude is 0.05 m, the frequency is 2 Π rad/s, and the stiffness of the spring is 285 N.m. Thus, the peak power output is approximately 14,000 mW for wave's amplitude and wave's frequency in the gulf of Thailand.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"42 12","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114109084","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 : 2017-05-01DOI: 10.1109/ICMSC.2017.7959494
Rong Yang, Yong Ma, Zhangzhi Tao, Rong Yang
During traditional route planning, the fighter is always seen as a point without considering the effect flying attitude, which results in the result of route planning is often rough and unusable. Since flying attitude of the fourth generation fighter affects its stealth heavily, this paper considers the effect of the flying attitude of the fourth generation fighter to route planning, and supposes that radar threaten can be avoided (when maximal probability detected by radar is less than 20%). Based on the above conditions, this paper gives stealthy route planning algorithm for the fourth generation fighter. Simulation results show the algorithm is reasonable, effective and usable.
{"title":"A stealthy route planning algorithm for the fourth generation fighters","authors":"Rong Yang, Yong Ma, Zhangzhi Tao, Rong Yang","doi":"10.1109/ICMSC.2017.7959494","DOIUrl":"https://doi.org/10.1109/ICMSC.2017.7959494","url":null,"abstract":"During traditional route planning, the fighter is always seen as a point without considering the effect flying attitude, which results in the result of route planning is often rough and unusable. Since flying attitude of the fourth generation fighter affects its stealth heavily, this paper considers the effect of the flying attitude of the fourth generation fighter to route planning, and supposes that radar threaten can be avoided (when maximal probability detected by radar is less than 20%). Based on the above conditions, this paper gives stealthy route planning algorithm for the fourth generation fighter. Simulation results show the algorithm is reasonable, effective and usable.","PeriodicalId":356055,"journal":{"name":"2017 International Conference on Mechanical, System and Control Engineering (ICMSC)","volume":"86 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114864299","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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