產(chǎn)品描述:
IMU-002慣性導航系統(tǒng)的出現(xiàn)滿足當今復雜的無人機和軍用飛機的性能要求,Yach工程師設計的IMU-002包括導航級的IMU慣性測量系統(tǒng)和包含卡爾曼濾波算法的INS/ GPS。,具有MEMS機電,符合包括溫度、沖擊、振動,電磁干擾、功率和濕度等等因素的MIL-STD環(huán)境要求,以適應惡劣的飛行環(huán)境。
產(chǎn)品優(yōu)勢:
1.提供精確的側(cè)傾、俯仰、航向數(shù)據(jù),在動態(tài)機動環(huán)境下可以持續(xù)轉(zhuǎn)彎
2.支持全大氣數(shù)據(jù)測量,包括AOA和側(cè)滑
3.支持寬容到GPS停運
4.可選軟件模塊支持最先進的全套飛行驗證,包括自動駕駛儀和導向、導航和任務管理功能
技術(shù)參數(shù):
|
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 |










