Tactical Grade High-Accuracy GNSS Inertial Navigation System For Vessel Tracking

Price	negotiable
MOQ	1
Delivery Time	2 week for sample
Brand	Firepower
Place of Origin	CHINA
Certification	CE
Model Number	INS100
Packaging Details	Wooden box
Payment Terms	L/C,T/T
Supply Ability	100/Month

Product Details

Product Specification

Place of Origin	CHINA	Gyro Bias Stability	≤0.3°/h(1σ)
Packaging Details	Wooden box	Gyro Bandwidth	300Hz
Model Number	INS100	Supply Ability	100/Month
Accelerometer Range	±50g	North Seeking Time	≤5min
Certification	CE	Brand Name	Firepower
Payment Terms	L/C,T/T	Gyro Range	±300°/s
Random Walk	0.05 °/h	Price	negotiable
Delivery Time	2 week for sample	Pitch Angle Holding Accuracy	≤0.2°/h
Scale Factor Nonlinearity	≤200ppm	Minimum Order Quantity	1

Product Description

Tactical Grade High-Accuracy GNSS Inertial Navigation System for Vessel Tracking

Product Description

INS-100 is a high-precision integrated navigation system designed for demanding applications requiring exceptional accuracy and reliability. It is equipped with three self-developed 40-grade fiber optic gyroscopes, tthree-self MEMS accelerometers, and advanced GNSS modules. By leveraging multi-sensor fusion and sophisticated integrated navigation algorithms, the system delivers precise positioning and navigation even in complex and dynamic environments.

With its high reliability and strong environmental adaptability, the INS-100 is suitable for a wide range of applications, including autonomous driving, unmanned aerial vehicles (UAVs), geospatial surveying and mapping, marine compasses, stabilized platforms, electro-optical pods, and underwater vehicles. Its robust design ensures stable and accurate performance across diverse operational conditions, making it an ideal choice for industries requiring superior navigation and motion-sensing capabilities.

Main functions of the integrated navigation system are as follows:

The initial alignment function is completed by using the output of the inertial device, and the shaking base alignment and the moving alignment can be carried out;
The GPS information received from outside can be used to complete the integrated navigation function and output information such as angle, speed and position.
After the satellite signal is lost, the inertial device output and the odometer input can be used to continue the navigation calculation;
It can output high performance and high sampling rate gyro raw output and add raw data for stable platform control.
The program and configuration parameters can be upgraded online through the serial port.

Main Parameters

Gyro technology

Project		Indicators	Remark
Gyro	Measuring range	-300°/s ~+300°/s
	Resolution	≤0.5°/h
	Bias residual	-1.0°/h ~+1.0°/h
	Random walk	0.05 o / h
	Biasstability at room temperature	≤0.3°/h(1σ)	10 seconds smoothing, 1H test result
	Biasstability at full temperature	≤0.5°/h(1σ)	10 seconds smoothing, 1H test result
	Normal-temperature Biasrepeatability	≤0.3°/h(1σ)	Statistics of 6 test data
	Biasrepeatability at full temperature	≤0.5°/h(1σ)	Take 2 Biasdata at full temperature, high temperature, low temperature and normal temperature respectively
	Scale factor nonlinearity	≤200ppm	Full temperature and constant temperature
	Scale factor repeatability	≤200ppm(1σ)	Full temperature and constant temperature
	Gyro start time	≤5s
	Gyro bandwidth	300Hz	Design assurance, batch testing
	Installation error residual of three-axis gyroscope	≤30"

Accelerometer technical indicators

Project		Indicators	Remark
Acceleration	Measuring range	-50g ~ +50g	Design and selection guarantee
	Scale factor nonlinearity	≤200ppm	Design and selection guarantee
	Biasstability at full temperature	≤100ug(1σ)	10 seconds smoothing, 1H test result
	Biasrepeatability at full temperature	≤100ug(1σ)	Take 2 Biasdata at full temperature, high temperature, low temperature and normal temperature respectively
	Scale factor repeatability	≤100ppm(1σ)	Design and selection guarantee
	Random walk	≤0.02m/s/h1/2
	Add up the starting time	≤5s
	Triaxial addition installation error residual	≤30"

Alignment accuracy

Integrated navigation accuracy (satellite effective)

Project		Indicators	Remark
Alignment accuracy	North seeking time	≤5min	Generally, the standard is 3min or 5min.
	Heading Angle Alignment Repeatability	≤1°/cosL	1σ
	Pitch Alignment Repeatability	≤0.05°	1σ
	Roll Angle Alignment Repeatability	≤0.05°	1σ
	North-seeking mode	Optional	It can realize swaying base alignment, GPS auxiliary alignment during travel, odometer auxiliary alignment during travel and main inertial navigation transfer alignment.

Inertial navigation accuracy (invalid satellite)

Project		Indicators	Remark
Inertial navigation accuracy	Accuracy of course angle maintenance	≤2°/h
	Pitch Angle Holding Accuracy	≤0.2°/h
	Accuracy of roll angle maintenance	≤0.2°/h
	Pure inertial positioning accuracy	≤20m(100s)	CEP, without external information assistance
	Position positioning accuracy of odometer integrated navigation	≤ 0.2% (mileage greater than 3 km)
	Position positioning accuracy of odometer integrated navigation	≤1m(50s)