Hom 58 laser gyroscope
KHOOM NTA
● Super siab ua haujlwm
● Built-in kub sensor tuaj yeem siv los them cov nqi gyro hauv lub sijhawm
●Nrog 25-pin hluav taws xob connector, lub gyroscope outputs ob TTL theem digital signals, uas yuav tsum tau txuas mus rau lub theem qhia, demodulation thiab suav circuits kom tau qhov yuav tsum tau angular displacement signals.
● Siv +15V, +5V thiab -5V DC fais fab mov
APPLICATION AREAS
●Marine platform compass
● Local reference
● Mid-range tactical missiles
● Nruab nrab qhov tseeb qhov chaw thiab kev taw qhia
● Helicopter
●Txoj kev coj cwj pwm
● Tus kheej-propelled artillery, torpedoes, thiab lwm yam.
PERMANCE Indicators
|
| Chav Kawm 1 | Chav kawm 2 | Chav kawm 3 |
| Zero Bias Stability | ≤ 0.01º / h | ≤ 0.015º / h | ≤ 0.02º / h |
| Zero Bias Repeatability | ≤ 0.01º / h | ≤ 0.015º / h | ≤ 0.02º / h |
| Random Wander | ≤ 0.002º / √h | ≤ 0.003º / √h | ≤ 0.005º / √h |
| Scale Factor | ≤ 5ppm (1σ) | ||
| Sib nqus Field Sensitivity | ≤ 0.004 º / h / Gs | ||
| Dynamic Range | ≤ ± 400 ° / S | ||
| Lub sijhawm pib | ≤10 秒 | ||
| MTBF | > 20000 小时 | ||
| Ua haujlwm kub | -40 ℃ ～ + 65 ℃ | ||
| Dimension | (85 ± 2) × (75 ± 2) × (52 ± 2) (mm) | ||
| Qhov hnyav | 620 ± 20 (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.) | ||
