SINS-003 strapdown inertial navigation system uses strap-down inertial components of flexible rate gyroscope and flexible accelerometer to measure the motion angular velocity and linear acceleration signal of the carrier along the axial.
Description:
Strapdown inertial navigation system uses inertial components of flexible rate gyroscope and flexible accelerometer to measure the movement angular velocity and linear acceleration signal of the carrier along the axial and to output aircraft navigation parameters, aircraft geography, navigation and body coordinate system.
Advantages:
1 The combination of inertia and carrier solid coupling, eliminating the need for a lot of electromechanical navigation platform, and a lot of convenience
2. Small size, low cost, gyroscopes and accelerometers account for only 1/7 of the navigation platform
3. Giving more navigation and guidance information
Applications:
Aircraft, aerospace fields
Technical Parameters:
|
Inertial Mode (Accuracy) |
|
|
Positioning |
20 Km |
|
Speed |
14 Km |
|
Heading |
0.5° |
|
Tilt and shake |
0.3° |
|
Conventional scope of use |
|
|
Interface |
RS422/485 |
|
Power supply |
27VDC |
|
Power |
14W |
|
Size |
240x160x110mm |
|
Weight |
3.4Kg |
|
Operating range |
|
|
Angular rate |
≤300°/sec |
|
Linear acceleration |
10g |
|
Vibration |
2000 Гц |
|
Operation Range |
-40℃ ~ +60℃ |
