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Honeywell-Equivalent Tactical-Grade IMU for Navigation & Positioning

Honeywell-Equivalent Tactical-Grade IMU for Navigation & Positioning

MOQ: 1 set
Price: $1000-$100000
Payment Method: T/T
Supply Capacity: 500 sets per year
Detail Information
Place of Origin
China
Brand Name
Wuhan Deep Pilot Technology Co.,Ltd.
Model Number
Inertial Measuring Unit Series
Product Description

The next-generation gyrocompassing-grade Inertial Measurement Unit (IMU) is engineered for demanding navigation, guidance, and precision positioning applications. Designed for mission-critical platforms, it delivers high-accuracy heading, attitude, and inertial navigation performance for aerospace, defense, unmanned systems, industrial surveying, and maritime operations.


The unit integrates a high-stability inertial sensor architecture within a rugged, environmentally sealed aluminum enclosure, ensuring superior resistance to vibration, shock, and harsh environmental conditions. Long-term drift stability is maintained without external cooling or auxiliary thermal management, reducing overall system burden.

This IMU is deployed across a wide range of platforms and operational environments, including:


  • UAV / VTOL flight control and autonomous navigation
  • UGV / USV / UUV robotic and unmanned systems
  • Weapon stabilization, targeting, and fire control systems
  • Maritime surveying and subsea exploration
  • Industrial drilling navigation and ground surveying
  • High-precision mapping & GIS platforms
  • Aerospace inertial navigation and GNSS-denied operations


Multiple electrical interface and output configurations are available for seamless integration with flight control computers, navigation processors, GNSS/INS fusion systems, avionics, and autonomous platforms. Users may configure output data rates, filtering profiles, and communication protocols to meet diverse mission requirements.


As a gyrocompassing-class inertial sensor, the system delivers high stability, high reliability, and excellent SWaP (Size, Weight, and Power) characteristics — providing advanced inertial navigation capability for GPS-denied or contested environments. It is ideally suited for applications requiring high-precision heading, inertial positioning, autonomous guidance, and long-duration navigation.


Parameter Specification
Navigation System Strapdown Inertial System (SINS)
Startup Time ≤ 10 s (from power-on to self-test completion)
Core Sensor Accuracy – Gyroscope Bias stability: ≤ 0.1°/h (1σ)
Bias repeatability: ≤ 0.05°/h (1σ)
Scale factor error: ≤ 20 ppm (1σ)
Random walk: ≤ 0.02°/√h (1σ)
Range: ±1000°/s
Core Sensor Accuracy – Accelerometer Bias stability: ≤ 5×10⁻⁵ g (1σ)
Bias repeatability: ≤ 5×10⁻⁵ g (1σ)
Scale factor error: ≤ 50 ppm (1σ)
Range: -60 g ~ +60 g
Navigation Data Update Rate ≥ 200 Hz
Input Voltage 18–32 V, typical 24 V
Power Consumption (Steady-State) ≤ 15 W
Weight ≤ 1.5 kg
Dimensions (D × H) 110 mm × 115 mm
Interfaces 1 × RS232, 1 × RS485, 1 × RS422
Operating Temperature -40 °C ~ +60 °C
Storage Temperature -55 °C ~ +70 °C
Operating Humidity ≤ 95% (25 °C)
Storage Humidity ≤ 95% (30 °C)



products
PRODUCTS DETAILS
Honeywell-Equivalent Tactical-Grade IMU for Navigation & Positioning
MOQ: 1 set
Price: $1000-$100000
Payment Method: T/T
Supply Capacity: 500 sets per year
Detail Information
Place of Origin
China
Brand Name
Wuhan Deep Pilot Technology Co.,Ltd.
Model Number
Inertial Measuring Unit Series
Minimum Order Quantity:
1 set
Price:
$1000-$100000
Payment Terms:
T/T
Supply Ability:
500 sets per year
Product Description

The next-generation gyrocompassing-grade Inertial Measurement Unit (IMU) is engineered for demanding navigation, guidance, and precision positioning applications. Designed for mission-critical platforms, it delivers high-accuracy heading, attitude, and inertial navigation performance for aerospace, defense, unmanned systems, industrial surveying, and maritime operations.


The unit integrates a high-stability inertial sensor architecture within a rugged, environmentally sealed aluminum enclosure, ensuring superior resistance to vibration, shock, and harsh environmental conditions. Long-term drift stability is maintained without external cooling or auxiliary thermal management, reducing overall system burden.

This IMU is deployed across a wide range of platforms and operational environments, including:


  • UAV / VTOL flight control and autonomous navigation
  • UGV / USV / UUV robotic and unmanned systems
  • Weapon stabilization, targeting, and fire control systems
  • Maritime surveying and subsea exploration
  • Industrial drilling navigation and ground surveying
  • High-precision mapping & GIS platforms
  • Aerospace inertial navigation and GNSS-denied operations


Multiple electrical interface and output configurations are available for seamless integration with flight control computers, navigation processors, GNSS/INS fusion systems, avionics, and autonomous platforms. Users may configure output data rates, filtering profiles, and communication protocols to meet diverse mission requirements.


As a gyrocompassing-class inertial sensor, the system delivers high stability, high reliability, and excellent SWaP (Size, Weight, and Power) characteristics — providing advanced inertial navigation capability for GPS-denied or contested environments. It is ideally suited for applications requiring high-precision heading, inertial positioning, autonomous guidance, and long-duration navigation.


Parameter Specification
Navigation System Strapdown Inertial System (SINS)
Startup Time ≤ 10 s (from power-on to self-test completion)
Core Sensor Accuracy – Gyroscope Bias stability: ≤ 0.1°/h (1σ)
Bias repeatability: ≤ 0.05°/h (1σ)
Scale factor error: ≤ 20 ppm (1σ)
Random walk: ≤ 0.02°/√h (1σ)
Range: ±1000°/s
Core Sensor Accuracy – Accelerometer Bias stability: ≤ 5×10⁻⁵ g (1σ)
Bias repeatability: ≤ 5×10⁻⁵ g (1σ)
Scale factor error: ≤ 50 ppm (1σ)
Range: -60 g ~ +60 g
Navigation Data Update Rate ≥ 200 Hz
Input Voltage 18–32 V, typical 24 V
Power Consumption (Steady-State) ≤ 15 W
Weight ≤ 1.5 kg
Dimensions (D × H) 110 mm × 115 mm
Interfaces 1 × RS232, 1 × RS485, 1 × RS422
Operating Temperature -40 °C ~ +60 °C
Storage Temperature -55 °C ~ +70 °C
Operating Humidity ≤ 95% (25 °C)
Storage Humidity ≤ 95% (30 °C)