MEMS加速度计
基于雾的惯性导航系统

适用于无人机、船舶和机载应用的高性能光纤陀螺仪惯性导航系统,精准、可靠、稳健

适用于无人机、船舶和机载应用的高性能光纤陀螺仪惯性导航系统,精准、可靠、稳健

本文是关于 IF4010 相关 FOG-40 型惯性测量单元的具体技术要求,该型惯性测量单元可广泛应用于车载、舰载、机载等领域。

  • 零件编号 :

    IF4010
  • 订单(最小起订量) :

    1
新产品
  • 描述

产品系列及参数

角速度测量的精度要求
角速度测量范围± 300 °/秒
室温零偏压稳定性(1σ 10秒平滑)≤ 0.8 °/h
高低温恒温零偏稳定性(1σ 10s 平滑)≤ 1.0 °C/小时
室温零偏差重复性(1σ):≤ 0.5 °/h
全温零偏差重复性(1σ):≤ 0.8 °/h;≤ 0.8 °/h;
室温下的非线性标度因子≤ 500ppm;
室温比例因子重复性≤ 300ppm;
陀螺仪带宽≥300Hz(设计保证)
陀螺仪精确启动时间10秒。
线性速度测量的精度要求
加速度测量范围± 20g(保证选择)(可选 50g 产品,精度略低);
室温零偏压稳定性(1σ 10秒平滑)≤ 200微克;
室温零偏差重复性(1σ)≤ 200微克;
开始时间10秒。
初始对准精度要求
初始对齐方法它可以执行振动台的初始对准、系泊系统的初始对准以及外部信息辅助航行的初始对准。
振动基座的初始自对准航向精度≤1.5° * secL(L 为当地纬度)
振动基座的初始自对准俯仰精度≤0.05°
振动基座的初始自对准滚动精度≤0.05°
底座摇晃的初始自对准时间5分钟(可进行自适应调整,建议系泊系统的初始对准时间为10分钟)
卫星故障时纯惯性导航指示器的要求
惯性导航航向角保持(漂移)精度≤1.5 °C/h(峰值)
惯性制导俯仰角保持(漂移)精度≤1.0 °/h(峰值)
惯性横滚角保持(漂移)精度≤1.0 °/h(峰值)
航向角测量范围0°~360°
仰角测量范围-90°~+90°
滚动角测量范围-180°~+180°
卫星有效组合导航指示器的要求
卫星综合导航航向角测量精度(足够的机动性)≤0.3°(1σ)
卫星集成导航(全机动)仰角测量精度:≤0.08°(1σ)
卫星集成导航(全机动)横滚角测量精度≤0.08°(1σ);
卫星综合导航水平定位精度(卫星单点定位,开放环境)≤1.5 米(1 σ)
5 卫星综合导航高程定位精度(卫星单点定位,开放环境)≤2.0 米(1 σ)
支持接收 RTCM3.X 数据,使卫星能够在 RTK 状态下运行。
支持双天线方向的可选产品。
环境适应性
工作温度适应性-40℃~+60℃
存储温度适应性-40℃~+60℃

生产过程


产品尺寸

FOG INS

 


应用场景

雾气 应用
基于光纤陀螺仪的惯性导航系统 适用于高精度导航和制导场景,例如: 无人机/垂直起降飞行器和飞机导航, 车辆/船舶姿态航向参考和GNSS/INS集成导航, 天线/雷达/光电稳定平台, 和 测量级移动测绘和地理配准—交付 超低漂移、优异的偏置稳定性以及强大的抗震/抗电磁干扰能力 适用于长时间高强度使用环境。
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MEMS accelerometer for UAV
无人机
MEMS accelerometer for robots
机器人
MEMS accelerometers are used in autonomous driving
自动驾驶

常问问题

问题1:IF4010惯性导航系统是用来做什么的?
答:IF4010是一款高性能光纤陀螺仪惯性导航系统,主要用于车载、舰载和机载应用。它提供精确的导航数据,例如角速度、线速度和定位信息。

Q2:IF4010系统的主要特点是什么?
A:高速输出角速度和线速度信息。
初始校准和自检功能。
卫星集成惯性导航。
能够在极端环境条件下运行(温度范围:-40°C 至 +60°C)。
设计紧凑轻巧,易于集成。
 
Q3:IF4010系统的精度是多少?
A:角速度精度:室温下≤0.8°/h。
线速度精度:室温下≤200μg。
航向角、俯仰角和横滚角精度:初始对准期间,航向角≤1.5°,俯仰角和横滚角≤0.05°。
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本文是关于 IF4010 相关 FOG-40 型惯性测量单元的具体技术要求,该型惯性测量单元可广泛应用于车载、舰载、机载等领域。
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