Accurate Gnss/Ins Integrated System for Uav Flight Control

• Customization: Available
• Type: Rockwell Hardness Tester
• Measuring Range: HB
• Application: Metal, Plastic, Ceramics and Glass, Stone
• Standard: ISO, ASTM, GB/T, BSEN
• Warranty: 3 Year
• Mobility: Desktop
• Calibrating Method: Standard Hardness Test Blocks
• Rated Voltage: 220V
• Support Language: Chinese
• Customized: Customized
• Self-North-Seeking Heading Accuracy: 0.06/Cosl1sigma)L Is The Local Latitude
• Speed Accuracy: 0.03m/S
• Customized Support: OEM
• Place of Origin: Guangdong,China
• Dimension: 178*178*134.5
• Material: Aluminum
• Size: 178*178*134.5
• Brand Name: Firepower
• Product Name: Integrated Inertial Navigation System
• Bandwidth: 200Hz
• Model Numbe: Ins300b
• Power: 18-36V
• Accuracy of Attitude Angle: 0.02 Measurement
• Operating Temperature: -40-+60
• Transport Package: Land Transport
• Specification: 78.0mm (L) × 78.0mm (W) × 80.0mm (H)
• Trademark: firepower
• Origin: Shenzhen

Product Description

Products Description

>Product features:

high precision, gyro accuracy 0.008(°)/h~0.015(°)/h(10s,1σ); gyro measurement range, ±500(°)/s, accelerometer measurement range ±20g, built-in multi-mode Satelite navigation system, the technical status of the shock absorber is optional.

>Typical applications: 1.Aircraft, ships, high-precision positioning and orientation

2.Unmannedaerial vehicles and unmanned ships 3.High-speed railinspection vehicle, coal mine inteligent roadheader, coal ming machine, digital map, 3D city modeling, etc.

Specification

PARAMETER			UNIT	INS-300A	INS-300B
Satellite navigation signal is valid
Self-north-seeking heading accuracy				≤0.03/cosL,(lσ) (Lis the local latitude)	≤0.06/cosL,(lσ) (Listhe local latitude)
Azimuth measurement accuracy			°	≤0.02,(1σ)	≤0.03,(1σ)
Accuracy of attitudeanglemeasurement				≤0.01,(1σ)	≤0.02,(1σ)
Speed accuracy			m/s	≤0.03
Position accuracy			m	≤2m(single point)/RTK2cm(CEP)
Satellite navigation signal loss effect
Satellite navigationsignal failure				≤0.02,1h(peak-to-peak value)	≤0.04,1h(peak-to-peak value)
Accuracy of attitude angle maintenance				≤0.02,1h(peak-to-peak value)	≤0.02,1h(peak-to-peak value)
Inertial horizontal position accuracy(airborne)			n mile	1.0(50%CEP,1h)	1.2(50%CEP,1h)
Inertialhorizontal position accuracy(on-board)			m	≤200(RMS,1h)	≤300(RMS,1h)
Inertial horizontal position accuracy(shipboard)			m	≤300(RMS,1h)	≤500(RMS,1h)
Horizontal position accuracy of inertial/DVL combination			m	0.2D%(Dis mileage)	0.3D%(Dis mileage)
Inertial/odometer combination horizontal position accuracy			m	0.1D%(Dis mileage)	0.15D%(Dis mileage)
System characteristics
North-seeking mode	Estimate latitude,shake base(GPS orodometer available)
Navigation mode	Pure Inertial,GPS Combination,Odometer Combination,Altimeter Combination,DVL Combination
1.Environmental parameters
Operating temperature				-40~+60
Storage temperature				-45~+75
Vibration			Hz,g²/Hz	20~2000,0.04
Impact			g,ms	20,11,half sine
2. Electrical parameters
Powersupply			V	+18~+36(DC)
Steady-statepower			W	≤25
Data interface			/	RS-422/CAN/network port
Data refresh rate			Hz	≤200(settable)
3. Physical parameters
Overall dimensions			mm	178*178*134.5
Installation dimensions			mm	162*162(4*Φ6.5)
Weight			kg	≤4.6

Details Images

Main Applications

Company Profile