IMU-001m惯导系统集成INS/GPS、大气数据套件以及多变量控制算法。
IMU-001m惯导系统在Yach工程师设计的设计下，产品带有完全集成化和微型化的飞行控制系统，该系统结合集成INS/GPS和完整强大的大气数据套件以及多变量控制算法。专为高性能、无人系统设计的 IMU-001m充分利用了LTi’zation设计技术，提供适用于各类强大的飞行控制算法。
产品详情 http://www.yach.com/p-1020.html
技术参数：
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SPECIFICATIONS |
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INS/GPS performance |
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Update rate |
100 Hz |
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Start-up time |
10 sec (initial attitude); 1 min (full alignment) |
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Heading range |
+/- 180° |
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Attitude accuracy |
0.3° (1 sigma)> |
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Altitude accuracy |
45 ft at S.L., <200 ft=""> at 40,000 ft altitude |
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Altitude range |
-1,000 ft to 50,000 ft |
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GPS antenna power |
5 V> |
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Airspeed accuracy |
<2 knots @ 40 knots, > <1 knot @ 60 knots> |
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Angle of attack range |
+/- 8° at max airspeed |
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Angle of sideslip range |
+/- 8° at max airspeed |
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Max airspeed |
120 knots standard, up to > 650 knots optional |
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IMU performance |
|
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Maximum angular rates |
+/- 200°/s |
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Maximum g range |
+/- 8 g |
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Environmental Specifications |
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Operating Temperature |
-40 to 70 ℃ |
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Non-operating temperature |
-54 to 85°C |
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Operating vibration/shock |
MIL-STD-810 |
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Humidity |
95%, non-condensing |
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