Hom 88 Laser Gyroscope
KHOOM NTA
● High precision
●Integrated tsim
● Built-in kub sensor, uas tuaj yeem siv los them tus nqi gyro hauv lub sijhawm.
● Nrog 37 core hluav taws xob connector, lub gyroscope outputs ob TTL theem digital signals, uas tuaj yeem txuas nrog rau theem kev txheeb xyuas, demodulation thiab suav circuits kom tau txais cov teeb liab xaim hluav taws xob xav tau.
● Siv +15V, +5V thiab -5V DC fais fab mov
APPLICATION AREAS
● Marine inertial navigation system
● High-precision tus cwj pwm ntsuas qhov system
● High-precision stabilization platform
●Stegic missiles, nruab nrab- thiab ntev-ntev tactical missiles
● Launcher thiab aerospace inertial kev taw qhia tshuab
● High-precision positioning thiab orientation systems
● High-precision av tsheb navigation system
PERMANCE Indicators
|
| Chav kawm I | Chav kawm 2 | Chav kawm 3 |
| Zero Bias Stability | ≤ 0.002º / h | ≤ 0.0025º / h | ≤ 0.003º / h |
| Zero Bias Repeatability | ≤ 0.002º / h | ≤ 0.0025º / h | ≤ 0.003º / h |
| Random taug kev | ≤ 0.0004º / √h | ≤ 0.0005º / √h | ≤ 0.0006º/√h |
| Scale Factor | ≤ 5ppm (1σ) | ||
| Sib nqus Field Sensitivity | ≤ 0.002 º / h / Gs | ||
| Dynamic Range | ± 400 ° / S | ||
| Lub sijhawm pib | ≤10 vib nas this | ||
| MTBF | > 20,000 teev | ||
| Ua haujlwm kub | -40 ℃ ～ + 65 ℃ | ||
| Dimension | (148 ± 2) × (126 ± 2) × (57 ± 2) (mm) | ||
| Qhov hnyav | 1900 ± 100 (g) | ||
| Kev siv fais fab | <5 W | ||
| poob siab | 75g, 6ms (ib nrab sine) | ||
| Kev vibration | ≤9.5g; (1300Hz ~ 1500Hz yog resonance point ntawm gyroscope, thiab resonance point ntawm A hom, B hom thiab C hom gyroscope yog txo nyob rau hauv kev txiav txim, uas yuav tsum tau zam nyob rau hauv cov qauv tsim ntawm inertial kev taw qhia system.) | ||
