产品形貌：
IMU-002惯性导航系统的泛起知足当今重大的无人机和军用飞机的性能要求 ，Yach工程师设计的IMU-002包括导航级的IMU惯性丈量系统和包括卡尔曼滤波算法的INS/ GPS 。 ，具有MEMS机电 ，切合包括温度、攻击、振动 ，电磁滋扰、功率和湿度等等因素的MIL-STD情形要求 ，以顺应卑劣的航行情形 。
产品优势：
1.提供准确的侧倾、俯仰、航向数据 ，在动态无邪情形下可以一连转弯
2.支持全大气数据丈量 ，包括AOA和侧滑
3.支持宽容到GPS停运
4.可选软件？橹С肿钕冉娜缀叫醒橹 ，包括自动驾驶仪和导向、导航和使命治理功效
手艺参数:
| SPECIFICATIONS | |
| INS/GPS performance | |
| Update rate | 100 Hz standard, configurable |
| Start-up time | 4 min |
| Heading range | +/- 180° |
| Attitude range pitch | +/- 90° |
| Attitude range roll | +/- 180° |
| Altitude range | -1,000 ft to 50,000 ft |
| Baroinertial altitude accuracy | 45 ft at S.L., 300 ft at > 50,000 ft altitude |
| GPS range | Worldwide |
| Lat/long position accuracy | 0.8 nmi/hr (1 sigma)> |
| Max airspeed | 200 knots standard |
| IMU performance (HG1700) | |
| Rate gyro bias | 1 or 3 deg/hr |
| Maximum g range | Maximum angular rates |
| Rate gyro bias | <0.003°/hr |
| Angular random walk | <0.002°/√hr |
| Reliability: MTBF | 20,000 hrs |
| Maximum angular rates | +/- 400°/s |
| Maximum g range | +/-20 g’s all axes |
| Pitch/roll accuracy, GPS aided | 0.02° rms |
| Heading accuracy, GPS aided | 0.1° rms |
| Pitch/roll accuracy, free inertial | 0.05° rms |
| Heading accuracy, free inertial | 0.1° rms |
| Environmental Specifications | |
| Operating Temperature | -40 to 70 ℃ |
| Temperature shock | MIL-STD-810 |
| Operating temperature at altitude | MIL-STD-810 |
| Operating vibration/shock | MIL-STD-810 |
