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TDF37IMU0 Fiber Optic Inertial Unit
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Introduction
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Overview
Fiber optic inertial units have the advantages of small size, light weight, low power consumption, and high accuracy. They can be used to design pure strapdown systems, meet the needs of new unmanned platforms, water/torpedo weapons, as well as land, airborne, and missile weapon platforms for small size and high-precision inertial unit equipment, and have dynamic measurement functions for carrier angular and linear motion information.
Performance
Project | Content | Index | Remark |
Performance indicators of gyroscope | |||
Zero bias indicator | Zero bias stability (10s) | 0.2°/h |
|
Variable temperature zero bias stability (100s) | 0.5°/h |
| |
Scale Factor | Scale factor nonlinearity | ≤20ppm |
|
Other indicators | random walk coefficient | 0.02°/√h |
|
input range | 400°/s |
| |
Performance indicators of accelerometer | |||
Deviation index | Zero bias repeatability | 0.3mg |
|
Zero bias indicator | Zero bias temperature sensitivity | 50μg/℃ |
|
Scale Factor | Scale factor repeatability | 300ppm |
|
Scale factor temperature sensitivity | 20ppm/℃ |
| |
Range indicator | input range | ±20g |
|
Whole machine characteristics | |||
Environmental performance indicators | operation temperature | -40℃~65℃ |
|
storage temperature | -40℃~60℃ |
| |
General requirements | power supply | 18~36V(DC) |
|
Stable power consumption | ≤8W | Startup power consumption ≤ 15W |
Dimensions
Weight: ≤ 0.5kg
信息为测试元素,使用时候可删除该元素放置自己想放的元素
这里是占位文字
信息为测试元素,使用时候可删除该元素放置自己想放的元素
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