Y. Korkishko, V. Fedorov, S. Prilutskiy, D. Obuhovich, I. Fedorov, V. Prilutskiy, V. Ponomarev, A. Zuev, V. Varnakov, I. Morev, S. Kostritskii
{"title":"紧凑型近导航级IFOG惯性测量单元IMU400","authors":"Y. Korkishko, V. Fedorov, S. Prilutskiy, D. Obuhovich, I. Fedorov, V. Prilutskiy, V. Ponomarev, A. Zuev, V. Varnakov, I. Morev, S. Kostritskii","doi":"10.1109/ISS50053.2020.9244909","DOIUrl":null,"url":null,"abstract":"At present time interferometric fiber-optic gyroscopes (IFOG, FOG) are widely used in inertial navigation systems (INS), and in wide range of applications have replaced its well-established main competitor ring laser gyroscopes (RLG). Recently, in order to cover the mass-market applications spectrum requiring low-cost and compact inertial sensor yet as much precise as it can be, RPC Optolink has launched new IFOG-based product: ultra-compact navigation-grade inertial measurement unit IMU400, its SWaP properties are: 80×95×62 mm, 0.7 kg, 0.5 l, ≤7 W. The aim of the current work was the production of IMU400 devices batches first, and then estimation of IMU 2019–2020 batches performance with direct approach and also with strapdown inertial navigation system (SINS) simulation methods, which is indirect way of performance observation, by its sense. Main IMU400 Gyro (FOG) and Accelerometer (ACC) parameters are: Angle Random Walk (ARW) = 0.007 °/√hour, Bias Instability (BI) = 0.01°/h; Velocity Random Walk (VRW) = 40μg/√Hz, BI = 6μg. SINS performance (best): heading 0.2°×sec(lat) (1σ, 10 min alignment time).","PeriodicalId":118518,"journal":{"name":"2020 DGON Inertial Sensors and Systems (ISS)","volume":"53 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-09-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Compact near-navigation-grade IFOG inertial measurement unit IMU400\",\"authors\":\"Y. Korkishko, V. Fedorov, S. Prilutskiy, D. Obuhovich, I. Fedorov, V. Prilutskiy, V. Ponomarev, A. Zuev, V. Varnakov, I. Morev, S. Kostritskii\",\"doi\":\"10.1109/ISS50053.2020.9244909\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"At present time interferometric fiber-optic gyroscopes (IFOG, FOG) are widely used in inertial navigation systems (INS), and in wide range of applications have replaced its well-established main competitor ring laser gyroscopes (RLG). Recently, in order to cover the mass-market applications spectrum requiring low-cost and compact inertial sensor yet as much precise as it can be, RPC Optolink has launched new IFOG-based product: ultra-compact navigation-grade inertial measurement unit IMU400, its SWaP properties are: 80×95×62 mm, 0.7 kg, 0.5 l, ≤7 W. The aim of the current work was the production of IMU400 devices batches first, and then estimation of IMU 2019–2020 batches performance with direct approach and also with strapdown inertial navigation system (SINS) simulation methods, which is indirect way of performance observation, by its sense. Main IMU400 Gyro (FOG) and Accelerometer (ACC) parameters are: Angle Random Walk (ARW) = 0.007 °/√hour, Bias Instability (BI) = 0.01°/h; Velocity Random Walk (VRW) = 40μg/√Hz, BI = 6μg. SINS performance (best): heading 0.2°×sec(lat) (1σ, 10 min alignment time).\",\"PeriodicalId\":118518,\"journal\":{\"name\":\"2020 DGON Inertial Sensors and Systems (ISS)\",\"volume\":\"53 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-09-15\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 DGON Inertial Sensors and Systems (ISS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ISS50053.2020.9244909\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 DGON Inertial Sensors and Systems (ISS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ISS50053.2020.9244909","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
摘要
目前,干涉式光纤陀螺仪(IFOG, FOG)在惯性导航系统(INS)中得到了广泛的应用,并取代了其主要竞争对手环形激光陀螺仪(RLG)。最近,为了覆盖需要低成本和紧凑的惯性传感器的大众市场应用频谱,RPC Optolink推出了新的基于ifog的产品:超紧凑导航级惯性测量单元IMU400,其SWaP特性为:80×95×62 mm, 0.7 kg, 0.5 l,≤7 W。本研究的目的是先批量生产IMU400器件,然后采用直接方法和捷联惯导系统(SINS)仿真方法对imu2019 - 2020批次进行性能估计,这是一种间接的性能观测方法。IMU400陀螺仪(FOG)和加速度计(ACC)的主要参数为:角度随机游走(ARW) = 0.007°/√h,偏置不稳定性(BI) = 0.01°/h;速度随机游走(Velocity Random Walk, VRW) = 40μg/√Hz, BI = 6μg。捷联惯导系统性能(最佳):航向0.2°×sec(后期)(1σ,对准时间10分钟)。
Compact near-navigation-grade IFOG inertial measurement unit IMU400
At present time interferometric fiber-optic gyroscopes (IFOG, FOG) are widely used in inertial navigation systems (INS), and in wide range of applications have replaced its well-established main competitor ring laser gyroscopes (RLG). Recently, in order to cover the mass-market applications spectrum requiring low-cost and compact inertial sensor yet as much precise as it can be, RPC Optolink has launched new IFOG-based product: ultra-compact navigation-grade inertial measurement unit IMU400, its SWaP properties are: 80×95×62 mm, 0.7 kg, 0.5 l, ≤7 W. The aim of the current work was the production of IMU400 devices batches first, and then estimation of IMU 2019–2020 batches performance with direct approach and also with strapdown inertial navigation system (SINS) simulation methods, which is indirect way of performance observation, by its sense. Main IMU400 Gyro (FOG) and Accelerometer (ACC) parameters are: Angle Random Walk (ARW) = 0.007 °/√hour, Bias Instability (BI) = 0.01°/h; Velocity Random Walk (VRW) = 40μg/√Hz, BI = 6μg. SINS performance (best): heading 0.2°×sec(lat) (1σ, 10 min alignment time).