FOG Strapdown Attitude Heading Reference System
The FOG Strapdown Attitude Heading Reference System consists of a closed-loop fiber optic gyroscope (ER-AHRS-10M uses an ultra-small closed-loop fiber optic gyroscope) and a quartz flexible accelerometer as the core inertial elements, aligned or initially self-aligned by the external input heading. The coordinated attitude system is realized through satellite signal combination correction the during flight. The product can work in a pure inertial attitude state or a satellite signal combined attitude state, and simultaneously output three-axis high-precision angular rate and linear acceleration signals (ER-AHRS-10 not combined). It can provide aircraft attitude, heading, position, speed, acceleration, angular velocity and other flight status parameters for cockpit display, aircraft control, radar antenna platform and other systems. It has the characteristics of small size, light weight, and high reliability.
Small and medium-sized general aircraft
1. What are the quotation methods?
If you have DHL or Fedex account, we can quote EXW price, otherwise CIF or FOB price.
2. Are there any discounts?
After we submit the sample price, if more quantity is needed, we will quote the bulk price.
3. How long will it take to deliver the goods after placing the order?
For sensors, parts and modules: in stock-one week; no stock-2-4 weeks; For systems, generally, 8-12 weeks.
4. How to deal with the quality problems?
After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.
If interested in FOG Strapdown Attitude Heading Reference System, pls contact us: email@example.com