INT-M-A05 Optical Gyroscope Aircraft Inertial Navigation System Drone UAVs 2000Hz Celestial RLG Inertial Positioning System Inertial Navigation System 

Detail Information

Place of Origin

China

Brand Name

INT

Model Number

INT-M-A05

Alignment Time:

≤5min

Position Accuracy/Pure Inertia:

≤2nm/1h,CEP

Position Accuracy/INS/GNSS Combination:

Better Than GNSS

Speed ​​accuracy/Pure Inertia:

≤1.5m/s,RMS

Speed ​​accuracy/INS/GNSS Combination:

≤0.2m/s,RMS

Heading Accuracy/Pure Inertia:

≤0.1°sec(L),RMS

Heading Accuracy/INS/GNSS Combination:

≤0.05°,RMS

Pitch & Roll Accuracy/Pure Inertia:

≤0.03°,RMS

Pitch & Roll Accuracy/INS/GNSS Combination:

≤0.02°,RMS

Dimensions:

130×130×110mm

Weight:

＜2.2kg

Temperature:

-40℃~60℃

Input Voltage:

DC24V(±25%)

Highlight:

gyroscope Aircraft Inertial Navigation System

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UAV Aircraft Inertial Navigation System

,

gyroscope inertial navigation system drone

Product Description

Aerospace FOG INS(INT-M-A05)

The airborne optical gyro inertial navigation system uses optical gyroscopes and quartz accelerometers as core sensors, employing strapdown or modulation technology systems. It operates advanced navigation software at high speeds internally, calculating and outputting navigation information in real-time. This series of products can integrate navigation information from satellites, astronomy, altimeters, radio, vision, etc., according to user needs, supporting pure inertial and multi-source information fusion working modes, providing users with comprehensive navigation information for the carrier.

    Applications: UAVs and special aircraft.

    Capabilities:

    1) Ground/air alignment;

    2) Alignment mode switching;

    3) Sensor fusion;

    4) Fault detection.

Series			Aerospace Inertial Navigation System(INS-A)
Type			INT-

M-A05
Accelerometer	Months Bias Repeatability(1σ)		≤30μg
	Months Scale Factor Accuracy(1σ)		≤30ppm
Gyro	Bias Repeatability(1σ)		≤0.01°/hr
	Scale Factor Accuracy(1σ)		≤30ppm
	Random walk(1σ)		≤0.005°/√hr
Features	Position Accuracy	Pure inertia	≤2nm/1h,CEP
		INS/GNSS combination	better than GNSS
	Speed Accuracy	Pure inertia	≤1.5m/s,RMS
		INS/GNSS combination	≤0.2m/s,RMS
	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time			＜5min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.1°sec(L),RMS
		INS/GNSS combination	≤0.05°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.03°,RMS
		INS/GNSS combination	≤0.02°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		130×130×110
	Weight		＜2.2kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞20000 hours