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2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)最新文献

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Integrity Enhancement of an Integrated Navigation System with Optical Sensors 光学传感器集成导航系统的完整性增强
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769400
P. Hecker, U. Bestmann, S. Wolkow, Maik Angermann, Andreas Dekiert
{"title":"Integrity Enhancement of an Integrated Navigation System with Optical Sensors","authors":"P. Hecker, U. Bestmann, S. Wolkow, Maik Angermann, Andreas Dekiert","doi":"10.23919/ICINS.2019.8769400","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769400","url":null,"abstract":"Vision-based navigation has been of interest in aviation for decades. Driven by the demand for optical verification of take-off and landing procedures during all-weather operation many developments have been raised following changes in technology of sensor and processing hardware and aviation requirements. This paper summarizes the developments from the 60s until today and exemplarily discusses aspects of vision-based augmentation of Integrated Navigation Systems (INS).","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"49 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116781814","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}
引用次数: 1
Passive Stabilization Systems for CubeSat Nanosatellites: General Principles and Features 立方卫星纳米卫星无源稳定系统:一般原理和特点
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769434
I. Belokonov, I. Timbai, D. Davydov
{"title":"Passive Stabilization Systems for CubeSat Nanosatellites: General Principles and Features","authors":"I. Belokonov, I. Timbai, D. Davydov","doi":"10.23919/ICINS.2019.8769434","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769434","url":null,"abstract":"This paper studies the dynamics of the angular motion of CubeSat nanosatellites with the passive stabilization systems of different types: aerodynamic, aerodynamic-gravitational, gravitational, gravitational-aerodynamic systems. The research was carried out in a probabilistic formulation. Using the obtained analytical distribution functions of the maximum angle of the nanosatellite longitudinal axis deviation from the required direction (orbital velocity vector, or local vertical), the formulas for selecting design parameters (geometrical dimensions, static stability margin, inertia moments) are derived. In the circular orbit at the required flight altitude, these parameters provide the deviation of the longitudinal axis from the required direction less than the allowable value with a given probability for a specified error of the initial angular velocity formed by the separation system. The nomograms for selecting the main design parameters of a CubeSat nanosatellite have been constructed.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"9 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115859978","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}
引用次数: 2
Quaternion Regular Equations and Algorithms of Space Inertial Navigation 空间惯性导航四元数正则方程与算法
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769350
Y. Chelnokov
{"title":"Quaternion Regular Equations and Algorithms of Space Inertial Navigation","authors":"Y. Chelnokov","doi":"10.23919/ICINS.2019.8769350","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769350","url":null,"abstract":"This paper proposes the new quaternion equations of perfect functioning for strapdown inertial navigation systems and for spatial inertial navigation systems with azimuthally stabilized platform and with the gyrostabilized platform which retains its orientation in an inertial reference frame. These equations use the regular four-dimensional variables proposed by the author of this paper. These INS equations are dynamically analogous to the quaternion regular equations of perturbed spatial two-body problem in four-dimensional Kustaanheimo-Stiefel variables, which makes it possible to use the results, obtained in the theory of regular celestial mechanics and astrodynamics, in space inertial navigation. This paper discusses the development of INS algorithms using the proposed quaternion equations of INS perfect functioning. This paper develops the results derived in [1]–[5].","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129324057","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}
引用次数: 2
Modeling of Scale Factor Nonlinear Distortions of Laser Gyro with Alternating Rectangular Bias 交变矩形偏置激光陀螺的比例因子非线性畸变建模
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769439
S.E. Beketov, N. I. Khokhlov, E. A. Petrukhin, V. Gorshkov, A. S. Bessonov
{"title":"Modeling of Scale Factor Nonlinear Distortions of Laser Gyro with Alternating Rectangular Bias","authors":"S.E. Beketov, N. I. Khokhlov, E. A. Petrukhin, V. Gorshkov, A. S. Bessonov","doi":"10.23919/ICINS.2019.8769439","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769439","url":null,"abstract":"The results of scale factor nonlinear distortion measurements related to the light backscattering effect in a laser gyro with a alternating rectangular bias are presented. It is shown that analytical relationships taking into account the conservative and dissipative backscattering components adequately describe a laser gyro frequency response in a wide working range of angular rotation velocities. The use of these relationships should reduce the values of nonlinear distortions down to 1–2 ppm by a proper scale factor correction.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"7 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128511583","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}
引用次数: 1
Mathematical Modeling of the Nonlinear Dynamics Components of Nanoelectromechanical Sensors taking into Account Thermal, Electrical and Noise Impacts 考虑热、电和噪声影响的纳米机电传感器非线性动力学元件的数学建模
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769406
I. Papkova, A. Krysko, M. Barulina, V. Krysko
{"title":"Mathematical Modeling of the Nonlinear Dynamics Components of Nanoelectromechanical Sensors taking into Account Thermal, Electrical and Noise Impacts","authors":"I. Papkova, A. Krysko, M. Barulina, V. Krysko","doi":"10.23919/ICINS.2019.8769406","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769406","url":null,"abstract":"A mathematical model of the vibrations of nanoelectromechanical sensors components as a nanobeam connected to an electrode at small distance was built. Nano beam was in a stationary temperature field, under impact Casimir forces, transverse alternating load and additive color noise. Geometric nonlinearity was taken into account according to the theory of Karman. In the particular case of the dependence of the Casimir force - deflection for elastic preheated beams have been studied.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"2 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134522260","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}
引用次数: 2
Research on Criteria for the Degree of Controllability of the State Variables of Dynamic Systems Models 动态系统模型状态变量可控性程度判据研究
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769427
M. Selezneva, K. Neusypin, I. V. Muratov
{"title":"Research on Criteria for the Degree of Controllability of the State Variables of Dynamic Systems Models","authors":"M. Selezneva, K. Neusypin, I. V. Muratov","doi":"10.23919/ICINS.2019.8769427","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769427","url":null,"abstract":"Approaches to solving problems of determining the degree of controllability of state variables of linear dynamic systems models are considered. The numerical criteria for calculating the degree of controllability of the state vector components are investigated. A numerical criterion for the degree of controllability of dynamic systems state variables is presented. An example of the practical use of the criterion in the problem of identify the most-effective-for-controlling parts of the flight path of an unmanned aerial vehicle is investigated.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"34 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134590435","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}
引用次数: 2
Estimating the Inertial Characteristics of a Nanosatellite Using a Radio Compass Based on GNSS Technology 基于GNSS技术的无线电罗盘估计纳米卫星惯性特性
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769358
A. Kramlikh, I. Lomaka, S. Shafran
{"title":"Estimating the Inertial Characteristics of a Nanosatellite Using a Radio Compass Based on GNSS Technology","authors":"A. Kramlikh, I. Lomaka, S. Shafran","doi":"10.23919/ICINS.2019.8769358","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769358","url":null,"abstract":"The paper describes a radio compass based on GNSS technology, an algorithm for processing GNSS information, an algorithm for calculating the coordinates of a unit vector of the longitudinal axis of a nanosatellite, and an approach that allows an estimation of the inertial characteristics of a nanosatellite. The estimation of the influence of the baseline length on the accuracy of determining the orientation angles is given. The results of the statistical study of the error determination of the nanosatellite inertial parameters using a radio compass are presented.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132687255","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}
引用次数: 1
The Use of a Genetic Algorithm for Parameter Adjustment of the Multi-Hypothesis Aircraft Tracking Algorithm 利用遗传算法对多假设飞机跟踪算法进行参数调整
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769413
D. Bedin, A. Ivanov
{"title":"The Use of a Genetic Algorithm for Parameter Adjustment of the Multi-Hypothesis Aircraft Tracking Algorithm","authors":"D. Bedin, A. Ivanov","doi":"10.23919/ICINS.2019.8769413","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769413","url":null,"abstract":"In previous studies, we developed a multi-hypothesis algorithm for the aircraft tracking, which shows good performance in the processing of real and model data. The algorithm operation depends on a large number of parameters. It is quite difficult to detect the influence of some parameters on the results. In this situation, it is justified to use a genetic algorithm to adjust the parameters.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"148 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114220062","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}
引用次数: 3
Modification of the Federated Kalman Filter Using the Observability Degree Criterion of State Variables 基于状态变量可观察度准则的联邦卡尔曼滤波器的改进
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769385
M. Selezneva, A. Proletarsky, K. Neusypin, Zhang Lifei
{"title":"Modification of the Federated Kalman Filter Using the Observability Degree Criterion of State Variables","authors":"M. Selezneva, A. Proletarsky, K. Neusypin, Zhang Lifei","doi":"10.23919/ICINS.2019.8769385","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769385","url":null,"abstract":"The implementation schemes of the federated Kalman filter are considered. It is proposed to increase the accuracy of the federated Kalman filter using a numerical criterion for the observability degree of state variables of the process assessed. The observability degree criterion is used to determine the correction factors of the federated Kalman filter. The effectiveness of the developed modifications of the federated Kalman filter is demonstrated by the example of estimating the errors of the aircraft inertial navigation system.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"99 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117179928","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}
引用次数: 5
Coriolis Vibratory Gyroscope with a Metal Resonator for Free Wave Mode 具有自由波模式金属谐振器的科里奥利振动陀螺仪
2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2019-05-01 DOI: 10.23919/ICINS.2019.8769368
V. Raspopov, V. V. Likhosherst, I. A. Volchikhin, V. V. Matveev, A. Ladonkin, S. I. Shepilov
{"title":"Coriolis Vibratory Gyroscope with a Metal Resonator for Free Wave Mode","authors":"V. Raspopov, V. V. Likhosherst, I. A. Volchikhin, V. V. Matveev, A. Ladonkin, S. I. Shepilov","doi":"10.23919/ICINS.2019.8769368","DOIUrl":"https://doi.org/10.23919/ICINS.2019.8769368","url":null,"abstract":"The dynamics of a coriolis vibratory gyroscope with a metal resonator in the free wave mode is considered in the paper. The envelopes of damping oscillations are given for excitation with a different amplitude at the resonant frequency. It is shown that with an increase in the amplitude of excitation, the interval of time to reach the boundary band, at which the signal can be separated from the noise, expands. The nonlinear character of the excitation transfer coefficient of the resonator is established.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"236 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123892228","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}
引用次数: 2
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