Y. Korkishko, V. Fedorov, V. Prilutskiy, V. Ponomarev, S. Prilutskiy, D. Obuhovich, I. Fedorov, A. Zuev, V. Varnakov, S. Kostritskii, I. Morev
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引用次数: 2
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。本研究的目的是批量生产中试IMU400装置,并采用直接方法和捷联惯导系统(SINS)仿真方法对IMU400的性能进行估计,从意义上说,捷联惯导系统是一种间接的性能观测方法。IMU400陀螺仪和加速度计的主要参数为:角度随机漫步(ARW) = 0.007°/√h,偏置不稳定性(BI) = 0.01°/h;流速随机游走(Velocity Random Walk, VRW) = 40µg/√Hz, BI = 6µg。捷联惯导系统预期性能(最大):航向0.2°×sec(后期)(1σ,对准时间10分钟)。
Ultra-compact navigation-grade 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 pilot IMU400 devices batch and the estimation of the performance of IMU with direct approach and also with strapdown inertial navigation systems (SINS) simulation methods, which by sense is indirect way of performance observation. Main IMU400 Gyro and Accelerometer parameters are: Angle Random Walk (ARW) = 0.007 °/√hour, Bias Instability (BI) = 0.01°/h; Velocity Random Walk (VRW) = 40µg/√Hz, BI = 6µg. SINS expected performance (max): heading 0.2°×sec(lat) (1σ, 10 min align time).