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Equivalent to Honeywell IMU for Advanced Navigation and Positioning

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Equivalent to Honeywell IMU for Advanced Navigation and Positioning

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 set per year

Details Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

L30 IMU

Startup Time:

≤ 10 S (from Power-on To Self-test Completion)

Gyroscope Bias Stability:

≤ 0.1°/h (1σ)

Gyroscope Bias Repeatability:

≤ 0.05°/h (1σ)

Gyroscope Scale Factor Error:

≤ 20 Ppm (1σ)

Gyroscope Range:

±1000°/s

Accelerometer Bias Stability:

≤ 5×10⁻⁵ G (1σ)

Accelerometer Bias Repeatability:

≤ 5×10⁻⁵ G (1σ)

Accelerometer Scale Factor Error:

≤ 50 Ppm (1σ)

Accelerometer 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)

Product Description

The next-generation gyrocompassing-grade Inertial Measurement Unit (IMU) is engineered for demanding navigation 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 advanced inertial sensing architecture within a rugged, environmentally-sealed aluminum enclosure, providing exceptional resistance to vibration, shock, and harsh environmental conditions. It maintains long-term performance stability without the need for external cooling or auxiliary thermal management.

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

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

Multiple interface and output configurations are available to support flexible integration into flight control computers, navigation computers, GNSS/INS integrated solutions, and avionics architectures. Users can configure output data rates, filtering modes, and communication protocols to optimize performance for specific mission profiles.

As a gyrocompassing-class inertial sensor, the unit offers high stability, high reliability, and excellent SWaP (Size, Weight, and Power) characteristics — providing advanced inertial navigation capability with reduced system burden. It is well-suited for applications requiring high-precision heading, inertial positioning, and sustained autonomy in GPS-denied or contested environments.

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)

Tags:

Products

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 set per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

L30 IMU

Startup Time:

≤ 10 S (from Power-on To Self-test Completion)

Gyroscope Bias Stability:

≤ 0.1°/h (1σ)

Gyroscope Bias Repeatability:

≤ 0.05°/h (1σ)

Gyroscope Scale Factor Error:

≤ 20 Ppm (1σ)

Gyroscope Range:

±1000°/s

Accelerometer Bias Stability:

≤ 5×10⁻⁵ G (1σ)

Accelerometer Bias Repeatability:

≤ 5×10⁻⁵ G (1σ)

Accelerometer Scale Factor Error:

≤ 50 Ppm (1σ)

Accelerometer 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)

Minimum Order Quantity:

1 set

Price:

$1000-$100000

Delivery Time:

30 work days

Payment Terms:

Supply Ability:

500 set per year

Product Description

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

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

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)

Tags:

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