TY-INS01A
Pure InertialHorizontalAccuracy(3σ,180s):≤180m
Pure InertialElevationAccuracy(3σ,180s):≤180m
Pure Inertial Heading Angle Accuracy(3σ,180s):≤0.2°
Pure Inertial Attitude Angle Accuracy(3σ,180s):≤0.1°
Weight≤1.5kg
外形Dimensions:211mm×65mm×120mm">
TY-INS01A
Fiber Optic Inertial Products
Product Introduction
The TY-INS01A inertial measurement unit measures the angular velocity and acceleration of the carrier through its internal inertial measurement unit, calculates the carrier's attitude, velocity, and position information. When satellite navigation data is valid, it performs integrated navigation and outputs high-precision attitude, velocity, and position information in real-time. It adapts to harsh mechanical environments and can be applied to unmanned aerial vehicles such as missiles, rockets, and drones.
Product Composition
The TY-INS01A inertial measurement unit consists of a tri-axis integrated fiber optic gyroscope, quartz flexure accelerometer, high-precision signal conversion circuit, navigation computer, power conversion circuit, vibration damping system, and interface circuit, etc.
Product Functions
· Equipped with self-test function;
· Equipped with inertial measurement function, outputting three-axis angular velocity and three-axis acceleration;
· Equipped with horizontal attitude angle initial alignment function;
· Equipped with transfer alignment function;
· Equipped with attitude measurement function, outputting pitch angle, roll angle, yaw angle and other information.
Technical Indicators
|
Category |
Technical Indicators |
Achieved Indicators |
|
Measurement Range |
Heading Angle Range |
0°~360° |
|
Pitch Angle Range |
±90° |
|
|
Roll Angle Range |
±180° |
|
|
Angular Velocity Measurement Range |
±500°/s |
|
|
Acceleration Measurement Range |
±30g |
|
|
Transfer Alignment Time |
Fast Alignment |
≤18s |
|
Fine alignment |
≤180s |
|
|
Self-Alignment Accuracy |
Attitude Angle Alignment Accuracy |
≤0.15 (3σ) |
|
Transfer Alignment Accuracy |
Heading Angle Alignment Accuracy |
≤0.05 (1σ) |
|
Attitude Angle Alignment Accuracy |
≤0.03 (1σ) |
|
|
Pure Inertial Navigation Accuracy |
Horizontal Position Accuracy |
≤180m (3σ, 180s) |
|
Altitude accuracy |
≤180m (3σ, 180s) |
|
|
Heading Angle accuracy |
≤0.2° (3σ, 180s) |
|
|
Attitude Angle Accuracy |
≤0.1° (3σ, 180s) |
|
|
Gyroscope Performance |
Bias Stability |
≤0.15°/h (1σ, 10s smoothing) |
|
Bias Repeatability |
≤0.1°/h (1σ) |
|
|
Accelerometer Performance |
Bias Stability |
≤0.15mg (1σ, 10s smoothing) |
|
Bias Repeatability |
≤0.1mg (1σ) |
|
|
Other Indicators |
Power Supply |
DC18V-34V |
|
Product Power Consumption |
Steady-State Power Consumption ≤18W |
|
|
Main Unit Weight |
≤1.5kg |
|
|
External Dimensions |
211mm×65mm×120mm |
|
|
Installation Dimensions |
193mm×40mm (4×φ5.5mm) |
版權(quán)所有:Copyright ? 2050 重慶天箭慣性科技股份有限公司 All Rights Reserved 備案號(hào):渝ICP備17008919號(hào)-1 -技術(shù)支持:網(wǎng)潤(rùn)軟件