Attitude And Heading Reference System Microelectromechanical Systems Small Volume And Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions For Unman
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MH-TY421 is a low cost system which can be used in simple vehicle navigation “Satcom on the move”antenna platform stabilization. This MEMS gyro,MEMS accelerometer, as well asalgorithmsuitable for conical scanning of antenna and satellite data correction this system uses, makes the requirement of hardware reduce greatly. Finally, the combination of dual antenna GPS or magnetometer can provideprecise navigation and position info for users. (1)Auto-output of navigation information (2)Meet the requirement of accurate measurement of attitude angleof aircraft, when in large maneuver flightand hovering. (3)Small volume and weight. (4)Communication interfaceRS422、CAN, to be selectable. (5)Wide voltage input range. (6)Can complete redevelopmentaccording to customers’requirement. Item Grade Remark System 1 Preparation time ≤2min 2 Attitude accuracy ≤1° 1σ(static) ≤2° 1σ(dynamic) 3 Heading accuracy ≤0.2°/ Baseline(GPS combined) ≤0.5°Magnetometer combined 4 Height accuracy 10 m (GPS combined) 5 Horizontal position accuracy 10m (CEP)(GPS combined) 6 Velocity accuracy Environment suitability 7 Shock 30g 8 Working temperature -40℃～65℃ 9 Vibration Meet the vehicle vibration requirement of GJB150.16A-2009 Physics characteristics 10 Size 150*110*50mm 11 Weight ＜700g 12 Power supply 18VDC～36VDC 13 Working power dissipation 10W Interface characteristics 14 Interface RS232、RS422、CAN Selectable 15 MTBF ≥1500h 16 Data refresh rate 100Hz 17 Band rate 115200bps 18 Memory 32G customized (1)“Satcom on the move”antenna stabilization (2)Unmanned vehicles
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Laser Gyro Cavity Mirror High Precision|ultra Smooth|laser Gyro|inertial Optical Component|precision Optics|prism For Ring Laser Gyroscope
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Wedged Mirror High Precision|ultra Smooth|laser Gyro|inertial Optical Component|precision Optics|prism For Ring Laser Gyroscope
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