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| Categories | Accelerometer Sensor |
|---|---|
| Brand Name: | KACISE |
| Model Number: | KSINS014C |
| Certification: | CE |
| Place of Origin: | CHINA |
| MOQ: | 1PCS |
| Payment Terms: | L/C,D/A,D/P,T/T,MoneyGram,Western Union |
| Supply Ability: | 1000 Piece/Pieces per Week negotiable |
| Delivery Time: | 5-8 work days |
| Packaging Details: | each unit has individual box and all boxes are packed in standard packages or customers requests available |
| Position Accuracy: | 1nmile/12h |
| Pitch & Roll Accuracy: | <0.0013° |
| Heading Accuracy: | < 0.008° |
| Speed Accuracy: | <0.1m/s |
| Initialization Time: | <13min |
| Company Info. |
| Xi'an Kacise Optronics Co.,Ltd. |
| Verified Supplier |
| View Contact Details |
| Product List |
KSINS014C Dual-Axis Fiber Optic Rotating Inertial Navigation System
Product Introduction
The KSINS014 is a dual-axis rotating inertial navigation system
that uses high-precision fiber optic gyroscopes and quartz flexible
accelerometers to suppress navigation error divergence through
rotational modulation. It can output position, speed, attitude,
angular rate, linear acceleration and other information in real
time. . The system has reserved software and hardware interfaces
for satellite receivers and air pressure modules to facilitate user
selection. It has software and hardware interfaces for astronomical
navigation and visual navigation, and can realize multiple
switchable navigation modes of inertial/satellite/atmospheric
combinations to meet the needs of UAV attitude control and
Navigation and positioning requirements.
Feature
● Has long-endurance pure inertial high-precision navigation
function
● A variety of switchable navigation modes including
inertial/satellite/atmospheric combinations
● Good vibration-shock-heat composite environmental adaptability
● Has in-situ self-calibration maintenance function
● Have complete BIT design
Application
It can be applied to all types of large and medium-sized
long-endurance UAVs.
Technical Specifications
Parameter | KSINS014C | |
Performance indicators | Position Accuracy | 1nmile/12h |
Pitch & Roll Accuracy | <0.0013° | |
Heading Accuracy | < 0.008° | |
Speed Accuracy | <0.1m/s | |
Initialization Time | <13min | |
Mechanical/ electrical interface | Steady state power consumption at normal temperature(W) | <36 |
Power supply(V) | 18~32 | |
Output | RS-422,RS-232,CAN | |
Size(mm) | 180×228×247 | |
Weight(Kg) | <12.5 | |
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