IMU-003慣性導(dǎo)航系統(tǒng)為了滿足無(wú)人機(jī)和軍事應(yīng)用的需求,我們的工程師在設(shè)計(jì)時(shí)提供了全方位的自動(dòng)駕駛儀和任務(wù)管理功能,包括自動(dòng)著陸和導(dǎo)航路線。在自動(dòng)駕駛儀使用高度自動(dòng)化的控制合成技術(shù),從設(shè)計(jì)上保證在整個(gè)飛行包線的穩(wěn)定性和性能魯棒性,主要滿足最嚴(yán)格的環(huán)保要求,確保長(zhǎng)時(shí)間無(wú)故障使用和在整個(gè)溫度和海拔高度范圍內(nèi)系統(tǒng)的性能保證。它的小尺寸規(guī)格使得它安裝在戰(zhàn)術(shù)無(wú)人機(jī)上可以達(dá)到理想的控制系統(tǒng)解決方案。
產(chǎn)品優(yōu)勢(shì):
1.產(chǎn)品自帶的卡爾曼濾波算法提供了全程INS姿態(tài)解決方案
2.提供精確的側(cè)傾、俯仰數(shù)據(jù),在動(dòng)態(tài)環(huán)境下可以持續(xù)的轉(zhuǎn)動(dòng)
3.支持全大氣數(shù)據(jù)測(cè)量,包括AOA和側(cè)滑
4.支持自主車(chē)輛控制,集成傳感器組件
技術(shù)參數(shù):
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SPECIFICATIONS |
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INS/GPS performance |
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Update rate |
50 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 range pitch |
+/- 90° |
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Attitude range roll |
+/- 180° |
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Altitude range |
-2,000 ft to 50,000 ft> |
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Baroinertial altitude accuracy |
45 ft at S.L., 40,000 ft altitude> |
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GPS range |
Worldwide |
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Lat/long position accuracy |
GPS C/A Code; differential ready, WAAS-enabled> |
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Max airspeed |
165 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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Operating vibration |
-Provisioned for passive isolation, MIL-STD-810 |
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Serial input/output |
RS-422 |
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Humidity |
95%, non-condensing sealed enclosure |










