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DINS-A Single-axis Rotating Laser Gyroscope Inertial Navigation System
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Introduction
Accesories
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Product Introduction
DINS-A single-axis rotating laser gyroscope inertial navigation system is a high-performance inertial navigation and measurement equipment. DINS-A adopts high-precision laser gyroscope and quartz flexible accelerometer, and the system performance is significantly improved through high-precision error calibration, temperature compensation technology and single-axis rotating online self-calibration and error self-compensation technology. Electromagnetic shielding design, thermal balance design, vibration mode design, sealing design and strict manufacturing technology are adopted in the system to ensure excellent environmental adaptability.
Product features
High-precision two-frequency mechanically dithered laser gyroscope
On-line self-calibration and error self-compensation of single-axis rotation
Anti-disturbance traveling self-alignment
The input interface is rich, which supports the reference information access of satellite navigation system/odometer/Doppler log/electromagnetic log/altimeter/ultra-short baseline underwater acoustic positioning system.
There are various working modes, and the pure inertia/damping/integrated navigation mode can be selected automatically or manually according to the external reference information.
Excellent environmental adaptability
Military standard
Application Areas
High precision ship navigation
Navigation and positioning of underwater unmanned submersible
Positioning and orientation of artillery geodesic vehicle
Positioning and orientation of Missile Launch Vehicle
High-precision Attitude Measurement
Electrical Characteristics
Power supply:28VDC(18~36VDC), <100W
Communication:configurable serial ports (921600), Ethernet port, 2 CAN bus interfaces, Ethernet interface, 1 PPS interface, odometer pulse interface, maximum output frequency 1000Hz.
Physical Characteristics
Size: Φ480mm×520mm (diameter×height)
Weight: ≤62kg (without buffer base)
Measuring range
Angular velocity:±400deg/s
Acceleration:±15g
Operating Environment
Operating/Storage Temperature:
-40℃~+60℃/-55℃~+80℃
Vibration:1g Sine@5~50Hz
Normal operation/no damage under shock:30g@6ms/50g@11ms
Specifications
Heading(RMS) secLat
|
Pure inertia |
≤60arcsec |
Damping/combination |
≤30arcsec |
|
Roll、Pitch(RMS)
|
Pure inertia |
≤30arcsec |
|
Damping/combination |
≤15arcsec |
Position(CEP)
|
Pure Inertial |
≤2nm/48h |
Guided Combination |
≤2m |
|
Doppler Meter Damping |
≤1nm/48h |
|
Electromagnetic Meter Damping |
≤1.5nm/48h |
|
Odometer combination |
≤0.15‰D |
|
Velocity (RMS)
|
Pure Inertia |
≤0.6m/s |
Damping |
≤0.2m/s |
|
Combined |
≤0.1m/s |
|
Start-up time
|
|
|
Marine Marina |
≤12h |
|
Marine offshore |
≤12h with GNSS |
|
Land based static |
≤7min |
|
Land-based travelling |
≤15min with OD |
|
Heave(RMS) |
|
2.5cm or 2.5% |
信息为测试元素,使用时候可删除该元素放置自己想放的元素
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信息为测试元素,使用时候可删除该元素放置自己想放的元素
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