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2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)最新文献

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SpaceNaute®: HRG technological breakthrough for advanced space launcher inertial reference system SpaceNaute®:先进空间发射器惯性参考系统的HRG技术突破
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405891
F. Delhaye, J. Girault
{"title":"SpaceNaute®: HRG technological breakthrough for advanced space launcher inertial reference system","authors":"F. Delhaye, J. Girault","doi":"10.23919/ICINS.2018.8405891","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405891","url":null,"abstract":"Space launchers are demanding robust and highly accurate INS to stage or inject satellites precisely into orbit, especially when the goal is the supersynchronous elliptical geostationary transfer orbit. As European leader of inertial navigation, Safran Electronics & Defense masters all inertial technologies (Ring Laser Gyro, Fiber Optic Gyro and Hemispherical Resonator Gyro). In the frame of the preparation of the Ariane 6 development, a trade-off analysis to offer the most advanced Space Launcher INS lead to the SpaceNaute® inertial reference based on the HRG technology. After a deep selection process conducted by ArianeGroup under European Space Agency (ESA) supervision, SpaceNaute® was selected against RLG and FOG based solutions proposed by the competitors. This paper describes the unique SWaP (Size, Weight and Power) breakthrough of SpaceNaute®, unveils key performance characteristics of the selected inertial sensors for SpaceNaute® and how HRG benefits are capitalized into the product.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116193296","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: 6
Extension of navigation methods on the basis of the inertial approach 在惯性接近的基础上扩展导航方法
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405905
Y. Binder, Y. Litmanovich, T. Paderina
{"title":"Extension of navigation methods on the basis of the inertial approach","authors":"Y. Binder, Y. Litmanovich, T. Paderina","doi":"10.23919/ICINS.2018.8405905","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405905","url":null,"abstract":"The paper gives a brief review of the results of the alternative concept for the implementation of the Schuler principle applied to an object performing spatial maneuvering, developed by the authors in their previous publications. In the framework of the proposed approach, based on the construction of a single-channel inertial vertical (SIV) on two vectors (observable and the specific force vector), the solutions to other problems are considered and substantiated: dead reckoning (DR) with compensation for the motion acceleration effects using SIV data and odometer (or log) readings; autonomous DR correction for realization of the observable vector by a free gyroscope with equatorial orientation (FG-E); correction of the FG-E errors using position updates, providing a control of the heading error etc. The discussion is supplied with a large amount of simulation results.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"217 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116429981","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
Analytical and numerical study of differential error equations for autonomous strapdown INS functioning in normal geographic frame 正常地理框架下自主捷联惯导系统的微分误差方程分析与数值研究
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405913
M. Loginov, Y. Chelnokov
{"title":"Analytical and numerical study of differential error equations for autonomous strapdown INS functioning in normal geographic frame","authors":"M. Loginov, Y. Chelnokov","doi":"10.23919/ICINS.2018.8405913","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405913","url":null,"abstract":"This paper presents the results of analytical and numerical study of nonhomogeneous full (nonlinear) and linear (linearized) differential error equations for autonomous strapdown INS, functioning in the normal geographic frame, which were derived earlier by the authors of this paper. These equations form the tenth-order system of nonstationary differential equations for object's altitude, latitude and longitude errors, northerly, vertical and easterly components of object's relative velocity error, and the errors for Rodrigues-Hamilton (Euler) parameters, which describe the orientation of an object in the normal geographic frame. Analytical estimates of strapdown INS errors are derived. For the three particular cases of object's motion, the analytical solutions are derived for the linear nonhomogeneous differential error equations for strapdown INS, and the following formulas are obtained: exact explicit formulas, which express the roots of the sixth-order characteristic equations, which characterize the intrinsic dynamics of strapdown INS and its instability for those particular cases of object's motion, through the parameters of object's unperturbed motion; the formulas for the amplitudes, frequencies, initial phases of harmonic components of the laws of variation of the errors of object's altitude, latitude, longitude, relative velocity projections; the formulas for the exponents of exponential components of these errors, which characterize their decrease or increase over time (these formulas characterize intrinsic dynamics of the INS).","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123761927","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: 0
Integrated approach to the development of digital regulators for inertial sensory elements of modern strapdown inertial navigation systems and of corresponding control software 现代捷联惯导系统惯性传感元件数字式调节器及其控制软件的综合开发方法
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405927
D. Kalikhman, L. Kalikhman, V. I. Grebennikov, V. Turkin, A. A. Akmaev, A. Nikolaenko, D. S. Gnusarev
{"title":"Integrated approach to the development of digital regulators for inertial sensory elements of modern strapdown inertial navigation systems and of corresponding control software","authors":"D. Kalikhman, L. Kalikhman, V. I. Grebennikov, V. Turkin, A. A. Akmaev, A. Nikolaenko, D. S. Gnusarev","doi":"10.23919/ICINS.2018.8405927","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405927","url":null,"abstract":"The report considers the development of digital regulators for inertial sensory elements of modern strapdown inertial navigation systems — precision angular rate and apparent acceleration meters, as well as software for their control. Modern computer technologies and the component base of digital electronics allow for combining the development of functional electronics, software, and synthesis of regulators into a single development complex in conditions of modern production environment, which in turn makes it possible to automate the entire process directly at workstations.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"61 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117163928","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
Navigation sensors and systems in GNSS degraded and denied environments 2018: (Or how i learned to stop worrying about GPS) 2018年，GNSS中的导航传感器和系统退化和被拒绝的环境:(或者我是如何学会不再担心GPS的)
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405890
G. Schmidt
{"title":"Navigation sensors and systems in GNSS degraded and denied environments 2018: (Or how i learned to stop worrying about GPS)","authors":"G. Schmidt","doi":"10.23919/ICINS.2018.8405890","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405890","url":null,"abstract":"Position, velocity, and timing (PVT) signals from the Global Positioning System (GPS) are used throughout the world but the availability and reliability of these signals in all environments has become a subject of concern for both civilian and military applications. This presentation summarizes recent advances in navigation sensor technology, including GPS, inertial, and other navigation aids that address these concerns. Also addressed are developments in sensor integration technology with several examples described, including the Bluefin-21 system mechanization.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"36 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121712074","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
Optimization of multiroute scanning of geometrically complex sensing zones for spacecraft with optoelectronic observation equipment 航天器光电观测设备几何复杂感测区多航路扫描优化
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405941
Y. Gorelov, S. B. Danilov, L. V. Kurganskaya, A. I. Manturov, V. Yurin
{"title":"Optimization of multiroute scanning of geometrically complex sensing zones for spacecraft with optoelectronic observation equipment","authors":"Y. Gorelov, S. B. Danilov, L. V. Kurganskaya, A. I. Manturov, V. Yurin","doi":"10.23919/ICINS.2018.8405941","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405941","url":null,"abstract":"The article considers the problem of multiroute scanning of geometrically complex observation zones for spacecraft with optoelectronic observation equipment. The scan model of shooting route in “push broom” mode is formed. The main tasks for the optimization of multiroute scanning are set in terms of the theory of optimal covers.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"32 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114449419","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
Solid-state wave gyroscope ensuring the required accuracy parameters 固态波陀螺仪确保所需的精度参数
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405893
V. Raspopov, I. A. Volchikhin
{"title":"Solid-state wave gyroscope ensuring the required accuracy parameters","authors":"V. Raspopov, I. A. Volchikhin","doi":"10.23919/ICINS.2018.8405893","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405893","url":null,"abstract":"This article lists the requirements to the material of a resonator that provide the appropriate mechanical properties. Also, the source and the parameters values of a generated wave that provide the balance at all forms of mass defects distribution of a resonator are presented. The controller electronics' typical structure and the workplace equipment for manual balancing are described.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"9 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129414548","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
Calculation of the landing area for a small asymmetric martian probe under the action of the Magnus gyroscopic moment 马格纳斯陀螺仪力矩作用下小型非对称火星探测器着陆面积的计算
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405866
V. Lyubimov
{"title":"Calculation of the landing area for a small asymmetric martian probe under the action of the Magnus gyroscopic moment","authors":"V. Lyubimov","doi":"10.23919/ICINS.2018.8405866","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405866","url":null,"abstract":"The perturbed motion of a small descending asymmetric probe in the Martian atmosphere at arbitrary angles of attack is considered. The low-frequency nonlinear system of differential equations of probe motion relative to the center of mass is used. The aim of the work is to determine the size of the landing area of a small asymmetric probe to Mars under the action of the Magnus gyroscopic moment. It should be noted that numerical results of calculation of the probe landing area are obtained taking into account the moment of Magnus.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"80 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132855729","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
Aircraft high accuracy positioning during approach to a platform using laser system with the GNSS signals outage 在GNSS信号中断的情况下，飞机在接近平台时使用激光系统进行高精度定位
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405880
S. P. Gulevich, I. Sergushov, E. N. Skripal, A. Abakumov, I. K. Kuzmenko, D. Livshits, K. D. Shapovalova
{"title":"Aircraft high accuracy positioning during approach to a platform using laser system with the GNSS signals outage","authors":"S. P. Gulevich, I. Sergushov, E. N. Skripal, A. Abakumov, I. K. Kuzmenko, D. Livshits, K. D. Shapovalova","doi":"10.23919/ICINS.2018.8405880","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405880","url":null,"abstract":"The article describes the automatic landing system providing access to the selected site on the basis of identification of the underlying surface in real time. The task is difficult and the article contains the necessary accompanying materials.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"117 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133527329","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
Adaptive algorithm for processing data of an AHRS with two units of micromechanical gyroscopes 双微机械陀螺仪AHRS数据处理的自适应算法
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI: 10.23919/ICINS.2018.8405910
Q. Liang, Y. Litvinenko
{"title":"Adaptive algorithm for processing data of an AHRS with two units of micromechanical gyroscopes","authors":"Q. Liang, Y. Litvinenko","doi":"10.23919/ICINS.2018.8405910","DOIUrl":"https://doi.org/10.23919/ICINS.2018.8405910","url":null,"abstract":"The problem statement of the adaptive algorithm for processing data of an attitude and heading reference system (AHRS) with two micromechanical (MEMS) inertial measurement units (IMU) is formulated in this paper. The system prototype with the use of two units of MPU6050 is also developed here to evaluate the performance of the adaptive algorithm. Experiments results show the possibility of estimating the intensity of the system noise for gyro biases both on the static and dynamic bases. The errors in determining the attitude and heading angles do not exceed 8 degrees during one hour of autonomous operation, which in turn confirms the effectiveness of the considered adaptive algorithms.","PeriodicalId":243907,"journal":{"name":"2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"160 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114168827","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
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