{"title":"PRIMUS:用于多种应用的面向swap的imu","authors":"A. Lenoble, T. Rouilleault","doi":"10.1109/InertialSensors.2016.7745670","DOIUrl":null,"url":null,"abstract":"In many applications, Size, Weight and Power (SWAP) consumption are key drivers in the design of a gyrocompass. During the past decade, Safran Electronics & Defense (formerly known as Sagem) designed the Hemispherical Resonator Gyroscope (HRG), a low-size, low-weight and low-power consumption sensor with remarkable performance to achieve efficient North Finding and Keeping (NF/NK), but also navigation-based applications. Taking the most out of HRG's outstanding reliability by design, Safran is now manufacturing a whole IMU product line, based on its high-end vibrating gyro, associated with MEMS accelerometers and a miniaturized electronic board. Through a SWAP-oriented design, Primus inertial measurement units are able to fulfil the needs of a wide range of navigation applications. Indeed, navigation systems based on Primus IMUs have already demonstrated: i) Sub-mil North and vertical finding accuracy, for many applications, including e.g. targeting ii) Sub-Metric inertial (GNSS-free) position keeping for cartography and mapping applications iii) State of the art accuracy for land and marine navigation systems iv) Easy integration into a navigator, thanks to Primus' multiple interfaces (GPS, DVL, CAN Bus, odometer, barometer ...). This paper introduces the Primus IMU and presents: v) An overview of Safran's work on the Hemispherical Resonator Gyroscope vi) Characteristics of the Primus IMU product line: a SWAP-focused architecture vii) Examples of applications addressed by Primus IMU.","PeriodicalId":371210,"journal":{"name":"2016 DGON Intertial Sensors and Systems (ISS)","volume":"32 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"PRIMUS: SWAP-oriented IMUs for multiple applications\",\"authors\":\"A. Lenoble, T. Rouilleault\",\"doi\":\"10.1109/InertialSensors.2016.7745670\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In many applications, Size, Weight and Power (SWAP) consumption are key drivers in the design of a gyrocompass. During the past decade, Safran Electronics & Defense (formerly known as Sagem) designed the Hemispherical Resonator Gyroscope (HRG), a low-size, low-weight and low-power consumption sensor with remarkable performance to achieve efficient North Finding and Keeping (NF/NK), but also navigation-based applications. Taking the most out of HRG's outstanding reliability by design, Safran is now manufacturing a whole IMU product line, based on its high-end vibrating gyro, associated with MEMS accelerometers and a miniaturized electronic board. Through a SWAP-oriented design, Primus inertial measurement units are able to fulfil the needs of a wide range of navigation applications. Indeed, navigation systems based on Primus IMUs have already demonstrated: i) Sub-mil North and vertical finding accuracy, for many applications, including e.g. targeting ii) Sub-Metric inertial (GNSS-free) position keeping for cartography and mapping applications iii) State of the art accuracy for land and marine navigation systems iv) Easy integration into a navigator, thanks to Primus' multiple interfaces (GPS, DVL, CAN Bus, odometer, barometer ...). This paper introduces the Primus IMU and presents: v) An overview of Safran's work on the Hemispherical Resonator Gyroscope vi) Characteristics of the Primus IMU product line: a SWAP-focused architecture vii) Examples of applications addressed by Primus IMU.\",\"PeriodicalId\":371210,\"journal\":{\"name\":\"2016 DGON Intertial Sensors and Systems (ISS)\",\"volume\":\"32 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 DGON Intertial Sensors and Systems (ISS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/InertialSensors.2016.7745670\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 DGON Intertial Sensors and Systems (ISS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/InertialSensors.2016.7745670","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2
摘要
在许多应用中,尺寸、重量和功耗(SWAP)消耗是陀螺仪罗盘设计的关键驱动因素。在过去的十年中,赛峰电子与防务公司(前身为萨基姆)设计了半球形谐振陀螺仪(HRG),这是一种低尺寸,低重量和低功耗的传感器,具有卓越的性能,可实现高效的寻北和保持(NF/NK),也可用于基于导航的应用。赛峰集团在设计上充分利用了HRG卓越的可靠性,目前正以其高端振动陀螺仪为基础,与MEMS加速度计和小型化电路板相结合,生产一整套IMU产品线。通过面向swap的设计,Primus惯性测量单元能够满足广泛导航应用的需求。事实上,基于Primus imu的导航系统已经证明:i)亚米制北方和垂直查找精度,适用于许多应用,包括例如瞄准ii)亚米制惯性(无gnss)定位,用于制图和测绘应用iii)陆地和海洋导航系统的最先进精度iv)易于集成到导航仪中,这要归功于Primus的多个接口(GPS, DVL, CAN总线,里程表,气压计…)。本文介绍了Primus IMU,并介绍了:v)赛峰在半球形谐振陀螺仪方面的工作概述vi) Primus IMU产品线的特点:以swap为中心的架构vii) Primus IMU解决的应用示例。
PRIMUS: SWAP-oriented IMUs for multiple applications
In many applications, Size, Weight and Power (SWAP) consumption are key drivers in the design of a gyrocompass. During the past decade, Safran Electronics & Defense (formerly known as Sagem) designed the Hemispherical Resonator Gyroscope (HRG), a low-size, low-weight and low-power consumption sensor with remarkable performance to achieve efficient North Finding and Keeping (NF/NK), but also navigation-based applications. Taking the most out of HRG's outstanding reliability by design, Safran is now manufacturing a whole IMU product line, based on its high-end vibrating gyro, associated with MEMS accelerometers and a miniaturized electronic board. Through a SWAP-oriented design, Primus inertial measurement units are able to fulfil the needs of a wide range of navigation applications. Indeed, navigation systems based on Primus IMUs have already demonstrated: i) Sub-mil North and vertical finding accuracy, for many applications, including e.g. targeting ii) Sub-Metric inertial (GNSS-free) position keeping for cartography and mapping applications iii) State of the art accuracy for land and marine navigation systems iv) Easy integration into a navigator, thanks to Primus' multiple interfaces (GPS, DVL, CAN Bus, odometer, barometer ...). This paper introduces the Primus IMU and presents: v) An overview of Safran's work on the Hemispherical Resonator Gyroscope vi) Characteristics of the Primus IMU product line: a SWAP-focused architecture vii) Examples of applications addressed by Primus IMU.