TY-FINS-90Z
Pure InertialPosition Accuracy(RMS):≤1nm
Pure InertialVelocity Accuracy(RMS):≤0.6m/s
Pure InertialHeading Accuracy(1σ):≤0.01°
Pure InertialAttitudeAccuracy(1σ):≤0.01°
Weight:≤5kg
Dimensions:180mm×180mm×140mm">

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TY-FINS-90Z

Fiber Optic Inertial Products


TY-FINS-90Z
Pure InertialPosition Accuracy(RMS):≤1nm
Pure InertialVelocity Accuracy(RMS):≤0.6m/s
Pure InertialHeading Accuracy(1σ):≤0.01°
Pure InertialAttitudeAccuracy(1σ):≤0.01°
Weight:≤5kg
Dimensions:180mm×180mm×140mm
Technical Support

Product Introduction

TY-FINS-90Z positioning and orientation system adopts a standard three-axis integrated fiber optic gyroscope, quartz flexure accelerometer, and high-precision satellite receiver. It adopts advanced integrated navigation algorithms to achieve high-precision measurement of the attitude, velocity, and position of moving carriers. It adapts to complex electromagnetic environments and harsh mechanical environments and can be applied to navigation and attitude measurement of various aircraft, vehicles, and ships.

 

Product Composition

The TY-FINS-90Z positioning and orientation system mainly consists of high-precision three-axis fiber optic gyroscopes, high-precision three-axis quartz flexure accelerometers, vibration damping system, high-precision satellite receiver, navigation computer, high-precision signal conversion circuits, power conversion circuits, interface circuits, and navigation software.

Product Functions

· Equipped with the function of initial alignment under static and dynamic conditions;

· Equipped with inertial navigation function;

· Equipped with the function of providing high-precision satellite-based augmentation system (SBAS) differential GNSS information;

· Equipped with INS/GNSS integrated navigation function;

· Equipped with communication with user terminals function;

· Equipped with the function of correcting system installation errors by binding external parameters.

Technical Indicators

Category

Technical Indicators

Achieved Indicators

Measurement Range

Heading Angle Range

360°

Pitch Angle Range

±90°

Roll Angle Range

±180°

Angular Velocity Measurement Range

±500°/s

Acceleration Measurement Range

±20g

Static Base Self-Alignment Accuracy

Alignment Time

≤5min

Heading Angle Alignment Accuracy

≤0.06°×sec(Lat) (1σ, Lat is local latitude)

Attitude Angle Alignment Accuracy

≤0.01° (1σ)

Dynamic Base Self-Alignment Accuracy

Under satellite positioning conditions

Alignment Time

≤5min

Heading Angle Alignment Accuracy

≤0.02° (1σ)

Attitude Angle Alignment Accuracy

≤0.01° (1σ)

Pure Inertial Navigation Accuracy, 1h

Position Accuracy

≤1nm (RMS)

Velocity Accuracy

≤0.6m/s(RMS)

Heading Angle Holding Accuracy

≤0.01° (1σ)

Attitude Angle Holding Accuracy

≤0.01° (1σ)

Integrated Navigation Accuracy

(PDOP≤4)

Single Point Positioning Accuracy

Horizontal ≤2m, Vertical ≤5m(RMS)

RTK-assisted Positioning Accuracy (Optional)

Horizontal ≤2+1ppm×Dcm (RMS)

Vertical ≤5+1ppm×Dcm (RMS)

D is the baseline length in km

Velocity Accuracy

≤0.03m/s(RMS)

Heading Angle accuracy

≤0.06° (1σ)

Attitude Accuracy

≤0.01° (1σ)

Gyroscope Performance

Bias Stability

≤0.01°/h (1σ, 10s smoothing)

Bias Stability

≤0.003°/h (1σ, 100s smoothing)

Bias Repeatability

≤0.003°/h (1σ)

Random Walk

≤0.0005°/h1/2

Accelerometer Performance

Bias Stability

≤0.1mg (1σ, 10s smoothing)

Bias Stability

≤0.03mg (1σ, 100s smoothing)

Bias Repeatability

≤0.05mg (1σ)

Other Indicators

Power Supply

28V±4V

Product Power Consumption

Steady-State Power Consumption ≤40W, Transient Power Consumption ≤80W

Main Unit Weight

≤5kg

External Dimensions

180mm×180mm×140mm

Installation Dimensions

162mm×162mm (4×φ8.5mm)

Ingress Protection

IP66

 

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