Improving the modeling of the dynamics of an object of an ergatic system requires the development of rational mathematical models based on flexible modular software, design automation, testing, as well as improving methods for identifying and correcting models. With a sharp increase in the quality of computer systems, the relevance of the development of analytical methods for the study of complex dynamic systems, including for the decomposition and creation of a modular hierarchical structure, has only increased. Proceeding from this, in the work in the application to the development of aviation simulators, the criteria for evaluating the dynamic characteristics of the object by the operator during the normal functioning of the ergatic system are determined. The main attention is paid to the short-period component of the longitudinal motion. The expansion of the spatial motion into longitudinal and transverse is carried out in terms of the roots of the characteristic polynomial of the fourth order (an example is given). A graphical-analytical method for determining the roots of a characteristic polynomial has been developed; the calculation algorithm is presented (it was effectively used in the development of a number of simulators). When studying spatial motion, it is natural to divide into separate channels. The simulation characteristics of the simulators are determined based on the corresponding simulation characteristics for each of the channels. Root methods play a special role in such studies. We restrict ourselves to systems described on each of the channels by systems of ordinary differential equations. The formalization of the criteria for evaluating the dynamic characteristics of the object by the operator in the process of functioning of the ergatic system is carried out.
{"title":"Flight Dynamics Simulators of Modular Structure: Assessment of the Dynamic Characteristics of an Object","authors":"Budylina Eugenia, Danilov Alexander, Garkina Irina","doi":"10.1109/icmeas54189.2021.00037","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00037","url":null,"abstract":"Improving the modeling of the dynamics of an object of an ergatic system requires the development of rational mathematical models based on flexible modular software, design automation, testing, as well as improving methods for identifying and correcting models. With a sharp increase in the quality of computer systems, the relevance of the development of analytical methods for the study of complex dynamic systems, including for the decomposition and creation of a modular hierarchical structure, has only increased. Proceeding from this, in the work in the application to the development of aviation simulators, the criteria for evaluating the dynamic characteristics of the object by the operator during the normal functioning of the ergatic system are determined. The main attention is paid to the short-period component of the longitudinal motion. The expansion of the spatial motion into longitudinal and transverse is carried out in terms of the roots of the characteristic polynomial of the fourth order (an example is given). A graphical-analytical method for determining the roots of a characteristic polynomial has been developed; the calculation algorithm is presented (it was effectively used in the development of a number of simulators). When studying spatial motion, it is natural to divide into separate channels. The simulation characteristics of the simulators are determined based on the corresponding simulation characteristics for each of the channels. Root methods play a special role in such studies. We restrict ourselves to systems described on each of the channels by systems of ordinary differential equations. The formalization of the criteria for evaluating the dynamic characteristics of the object by the operator in the process of functioning of the ergatic system is carried out.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"22 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123502696","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00038
H. Ma, Zhen Lu, X. Zhang, W. Liao
The malfunction of attitude control system will lead to continuous attitude tumble of on-orbit spacecraft, which brings two problems to attitude estimation, one is the large initial error, and the other is the status mutation. Focusing on the above two issues, a robust strong tracking cubature Kalman filter (RSTCKF) is proposed in this paper to obtain the high-precision and real-time attitude knowledge of failed spacecraft. On the one hand, the multiplicative quaternion is adopted in the whole filter process instead of the additive one to keep the quaternion normalized, which increases the numerical stability of CKF; on the other hand, the time-varying multiple fading factors are introduced to adjust the different channels of prediction error covariance matrix, which strengthens the tracking ability of CKF to status mutation. Numerical simulations verify the effectiveness of the developed algorithm.
{"title":"Robust Strong Tracking Cubature Kalman Filter for Attitude Estimation of Failed Spacecraft","authors":"H. Ma, Zhen Lu, X. Zhang, W. Liao","doi":"10.1109/icmeas54189.2021.00038","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00038","url":null,"abstract":"The malfunction of attitude control system will lead to continuous attitude tumble of on-orbit spacecraft, which brings two problems to attitude estimation, one is the large initial error, and the other is the status mutation. Focusing on the above two issues, a robust strong tracking cubature Kalman filter (RSTCKF) is proposed in this paper to obtain the high-precision and real-time attitude knowledge of failed spacecraft. On the one hand, the multiplicative quaternion is adopted in the whole filter process instead of the additive one to keep the quaternion normalized, which increases the numerical stability of CKF; on the other hand, the time-varying multiple fading factors are introduced to adjust the different channels of prediction error covariance matrix, which strengthens the tracking ability of CKF to status mutation. Numerical simulations verify the effectiveness of the developed algorithm.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"28 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127933599","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00044
Liang Yan, Zhao Dongguo, Lu Xianguo, Jie Xiaoyuan, Wang Chenglin
We propose a new clustering method called LGKSC, which is an alternative model based on gravitational kinematics to simulate local synchronization. The difference from existing clustering algorithms is that the algorithm makes objects over time. The dynamics of interaction are gradually synchronized dynamically, forming a local cluster corresponding to the internal structure of the data set. LGKSC can determine clusters with any shape, size and density, and can identify the amount of clusters automatically. LGKSC can adaptively identify the neighbors of the data objects based on the Davies-Bouldin (DB) index, so it can choose the best clustering results. Experiments indicate that the proposed method may take more time to run, but the algorithm have advantages in detecting the amount and the accuracy of clusters.
{"title":"A Local Gravity Kinematics Synchronization Clustering Algorithm","authors":"Liang Yan, Zhao Dongguo, Lu Xianguo, Jie Xiaoyuan, Wang Chenglin","doi":"10.1109/icmeas54189.2021.00044","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00044","url":null,"abstract":"We propose a new clustering method called LGKSC, which is an alternative model based on gravitational kinematics to simulate local synchronization. The difference from existing clustering algorithms is that the algorithm makes objects over time. The dynamics of interaction are gradually synchronized dynamically, forming a local cluster corresponding to the internal structure of the data set. LGKSC can determine clusters with any shape, size and density, and can identify the amount of clusters automatically. LGKSC can adaptively identify the neighbors of the data objects based on the Davies-Bouldin (DB) index, so it can choose the best clustering results. Experiments indicate that the proposed method may take more time to run, but the algorithm have advantages in detecting the amount and the accuracy of clusters.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"59 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126610246","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00033
Lu Chenyu, Liang Xiaoyang, Zhou Zhitan, Le Guigao
In this paper, a four-nozzle liquid oxygen (LOX)/kerosene rocket is used to analyse the afterburning effects on the thermal environment of flame deflectors. Based on the three-dimensional compressible Reynolds-Averaged Navier-Stokes (RANS) equations and the realizable k-ε turbulence model, the rocket plume model is established. A 9-species,10-steps chemistry scheme is used for the simulation of afterburning reaction. On this basis, the impinging flow fields of the rocket exhaustjet with and without chemical reaction are calculated. The results show that the afterburning reaction mainly occurs in the tail section of the plume and the near-wall region, which will obviously increase the local gas temperature. Additionally, the temperature of the mixed layer of the plume also increases due to the afterburning reaction. For the deflector, the temperature of areas under the direct impingement of the rocket plume rises by 20% after adding the afterburning reaction. Meanwhile, a high-temperature layer will be formed, which will obviously increase the overall temperature of the deflector.
本文以四喷嘴液氧/煤油火箭为研究对象，分析了加力燃烧对转焰器热环境的影响。基于三维可压缩reynolds - average Navier-Stokes (RANS)方程和可实现的k-ε湍流模型，建立了火箭羽流模型。采用9种物质、10步化学方法模拟加力燃烧反应。在此基础上，计算了有化学反应和无化学反应时火箭排气射流的冲击流场。结果表明:加力燃烧反应主要发生在羽流尾部和近壁面区域，会明显提高局部气体温度;此外，羽流混合层的温度也因加力燃烧反应而升高。对于偏转板，加入加力反应后，火箭羽流直接撞击区域的温度升高了20%。同时，会形成高温层，使偏转板整体温度明显升高。
{"title":"Investigation of Afterburning Effects on the Thermal Environment of Flame Deflectors","authors":"Lu Chenyu, Liang Xiaoyang, Zhou Zhitan, Le Guigao","doi":"10.1109/icmeas54189.2021.00033","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00033","url":null,"abstract":"In this paper, a four-nozzle liquid oxygen (LOX)/kerosene rocket is used to analyse the afterburning effects on the thermal environment of flame deflectors. Based on the three-dimensional compressible Reynolds-Averaged Navier-Stokes (RANS) equations and the realizable k-ε turbulence model, the rocket plume model is established. A 9-species,10-steps chemistry scheme is used for the simulation of afterburning reaction. On this basis, the impinging flow fields of the rocket exhaustjet with and without chemical reaction are calculated. The results show that the afterburning reaction mainly occurs in the tail section of the plume and the near-wall region, which will obviously increase the local gas temperature. Additionally, the temperature of the mixed layer of the plume also increases due to the afterburning reaction. For the deflector, the temperature of areas under the direct impingement of the rocket plume rises by 20% after adding the afterburning reaction. Meanwhile, a high-temperature layer will be formed, which will obviously increase the overall temperature of the deflector.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"202 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123036409","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00030
Leonidas Quiroz, Jimmy W. Gallegos, Christian Montaleza, Oscar Arteaga, R. Cruz
This article focuses on the study of the regeneration of catalyst monolith metals used in gasoline vehicles, through the realization of the oxidation-reduction method at: controlled temperature, exposure time and constant flow of inert gases (N2 and H2). According to the size and shape of the monolith structure of the commercial 2-way and 3-way catalysts used for the test, rectangular samples with a weight of 4.125 g and a cubic cut with 20 mm edges were taken for the study. In addition, the emissions behavior of each of the gases after regeneration was analyzed by means of a gas analyzer incorporated directly to the reactor with the samples treated in a vehicle without catalytic converter, thus determining that through the oxidation-reduction process the species of the catalytic monolith are recovered. In this way, the catalytic process of transforming harmful emissions into harmless gases, product of the combustion processes of gasoline engines, is improved, thus reducing the environmental waste they produce after elimination. It should be noted that in simple processes, due to its ceramic structure and the presence of noble metals, its elimination is difficult.
{"title":"Regeneration of vehicle catalytic converters by metal treatment system in monoliths","authors":"Leonidas Quiroz, Jimmy W. Gallegos, Christian Montaleza, Oscar Arteaga, R. Cruz","doi":"10.1109/icmeas54189.2021.00030","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00030","url":null,"abstract":"This article focuses on the study of the regeneration of catalyst monolith metals used in gasoline vehicles, through the realization of the oxidation-reduction method at: controlled temperature, exposure time and constant flow of inert gases (N2 and H2). According to the size and shape of the monolith structure of the commercial 2-way and 3-way catalysts used for the test, rectangular samples with a weight of 4.125 g and a cubic cut with 20 mm edges were taken for the study. In addition, the emissions behavior of each of the gases after regeneration was analyzed by means of a gas analyzer incorporated directly to the reactor with the samples treated in a vehicle without catalytic converter, thus determining that through the oxidation-reduction process the species of the catalytic monolith are recovered. In this way, the catalytic process of transforming harmful emissions into harmless gases, product of the combustion processes of gasoline engines, is improved, thus reducing the environmental waste they produce after elimination. It should be noted that in simple processes, due to its ceramic structure and the presence of noble metals, its elimination is difficult.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"9 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124977833","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00018
Lijie Chen
The fundamental theory of generating coaxiality error graph is studied. A mathematical model for visualization of coaxiality error is established in accordance with the definition of coaxiality error in national standard. The theory of three-dimensional wireframe models on computer graphics is applied to realize the display of extracted derived feature and associated derived feature on the measured multi-diameter axle. Axonometric projection transformation is used to attain the realization of basic geometric shapes. The spacial hidden method is adopted to solve the problem of geometrical graph hidden. According to the above theoretical research, the corresponding software is developed on the LabWindows/CVI software platform to realize the visualization of coaxiality error.
{"title":"Mathematical Model on the Visualization of coaxiality Error","authors":"Lijie Chen","doi":"10.1109/icmeas54189.2021.00018","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00018","url":null,"abstract":"The fundamental theory of generating coaxiality error graph is studied. A mathematical model for visualization of coaxiality error is established in accordance with the definition of coaxiality error in national standard. The theory of three-dimensional wireframe models on computer graphics is applied to realize the display of extracted derived feature and associated derived feature on the measured multi-diameter axle. Axonometric projection transformation is used to attain the realization of basic geometric shapes. The spacial hidden method is adopted to solve the problem of geometrical graph hidden. According to the above theoretical research, the corresponding software is developed on the LabWindows/CVI software platform to realize the visualization of coaxiality error.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"52 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123324964","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00031
F. B. Teshome, Bei Peng, W. Ke, Fuguo Ge, X. Du, Z. Zeng
NiTi and Ti6A14V were materials with superior properties and shared application areas while joining them with fusion weld stayed as a challenge. Solidification of excessive brittle Ti2Ni intermetallic phases and development of microcracks are the main challenges of creating weld between these alloys. Therefore, Pulsed mode welding with an offset laser was employed to develop a dissimilar weld between NiTi and Ti6A14V with the aid of Cobalt and Zirconium interlayers. The involvement of interlayers along with laser offsetting improved the mechanical properties of the joint. Tensile strength of the joints with Zirconium and Cobalt interlayers reached a maximum of 319MPa and 275MPa with a percentage elongation of 1.53% and 1.47%, while the weld without interlayer was limited to 148MPa and 0.8%. A thermal transient model with a Modified Three-Dimensional Conical volumetric heat source was employed to predict the temperature distribution and Weld-pool shape in dissimilar NiTi/Ti6Al4V weld with and without the interlayers, and a good agreement was evident between simulated and experimental results.
{"title":"Prediction of Weld Pool Profile of Dissimilar Laser Weld Between NiTi/Ti6Al4V Via Different Interlayers","authors":"F. B. Teshome, Bei Peng, W. Ke, Fuguo Ge, X. Du, Z. Zeng","doi":"10.1109/icmeas54189.2021.00031","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00031","url":null,"abstract":"NiTi and Ti6A14V were materials with superior properties and shared application areas while joining them with fusion weld stayed as a challenge. Solidification of excessive brittle Ti2Ni intermetallic phases and development of microcracks are the main challenges of creating weld between these alloys. Therefore, Pulsed mode welding with an offset laser was employed to develop a dissimilar weld between NiTi and Ti6A14V with the aid of Cobalt and Zirconium interlayers. The involvement of interlayers along with laser offsetting improved the mechanical properties of the joint. Tensile strength of the joints with Zirconium and Cobalt interlayers reached a maximum of 319MPa and 275MPa with a percentage elongation of 1.53% and 1.47%, while the weld without interlayer was limited to 148MPa and 0.8%. A thermal transient model with a Modified Three-Dimensional Conical volumetric heat source was employed to predict the temperature distribution and Weld-pool shape in dissimilar NiTi/Ti6Al4V weld with and without the interlayers, and a good agreement was evident between simulated and experimental results.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"28 8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116720001","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00013
Yanjing Liu, Ruiting Li
With the tremendous improvement of industrial manufacturing, the methods and technology of automobile industry have made great progress. As a significant factor determining the appearance of vehicle models, the dimension control of body-in-white (BIW) also has constantly optimization in the continuous innovation of automotive products. The dimension control of BIW is of great importance in the production process and plays a connecting role in automobile manufacturing. As for actual BIW production, not only a complete body framework is established through the assembly of stamping parts, but also the hang-on parts are preliminarily installed and matched with the body framework to form the basis for the assembly of following parts. In this study, current researches and methods of BIW dimension control in automobile industry are summarized and illustrated. Then, factors which affecting the dimension status of BIW are classified and highlighted by main types. The model and system of process control based on data analysis are established. Finally, the model and strategy are sufficiently validated by test result.
{"title":"Multi-factor based analysis and statistical process control for body-in-white dimension status","authors":"Yanjing Liu, Ruiting Li","doi":"10.1109/icmeas54189.2021.00013","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00013","url":null,"abstract":"With the tremendous improvement of industrial manufacturing, the methods and technology of automobile industry have made great progress. As a significant factor determining the appearance of vehicle models, the dimension control of body-in-white (BIW) also has constantly optimization in the continuous innovation of automotive products. The dimension control of BIW is of great importance in the production process and plays a connecting role in automobile manufacturing. As for actual BIW production, not only a complete body framework is established through the assembly of stamping parts, but also the hang-on parts are preliminarily installed and matched with the body framework to form the basis for the assembly of following parts. In this study, current researches and methods of BIW dimension control in automobile industry are summarized and illustrated. Then, factors which affecting the dimension status of BIW are classified and highlighted by main types. The model and system of process control based on data analysis are established. Finally, the model and strategy are sufficiently validated by test result.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"3 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127093141","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00047
Xiaobin Huang, Yan Zhang, Rui Xiao
Space target orbit determination module is an important component of space target surveillance radar system. The development of this module requires very complex aerospace dynamics knowledge, which brings great difficulties to non-orbit mechanics researchers engaged in radar system design. The core of orbit determination is the calculation of perturbation acceleration, which is the basis of high precision numerical orbit calculation. To this end, this paper takes the atmospheric drag perturbation which can not be ignored in the precise orbit determination of LEO satellite as an example, introduces its mathematical principle, gives the program design idea and function interface implementation, and makes a simulation comparison with STK. The experimental results verify the effectiveness of the interface function, and show that the function interface designed in this paper can assist researchers in radar system design.
{"title":"Analysis of Atmospheric Drag Acceleration and Engineering Realization of Space Target","authors":"Xiaobin Huang, Yan Zhang, Rui Xiao","doi":"10.1109/icmeas54189.2021.00047","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00047","url":null,"abstract":"Space target orbit determination module is an important component of space target surveillance radar system. The development of this module requires very complex aerospace dynamics knowledge, which brings great difficulties to non-orbit mechanics researchers engaged in radar system design. The core of orbit determination is the calculation of perturbation acceleration, which is the basis of high precision numerical orbit calculation. To this end, this paper takes the atmospheric drag perturbation which can not be ignored in the precise orbit determination of LEO satellite as an example, introduces its mathematical principle, gives the program design idea and function interface implementation, and makes a simulation comparison with STK. The experimental results verify the effectiveness of the interface function, and show that the function interface designed in this paper can assist researchers in radar system design.","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132011590","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 : 2021-10-01DOI: 10.1109/icmeas54189.2021.00006
{"title":"Message from Program Chair","authors":"","doi":"10.1109/icmeas54189.2021.00006","DOIUrl":"https://doi.org/10.1109/icmeas54189.2021.00006","url":null,"abstract":"","PeriodicalId":374943,"journal":{"name":"2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131253264","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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