INERTIAL SENSORS  -  MEMS Angular Rate Sensors

QRS11-00100-100/101

QRS14-0xxxx-102/103

HZ1-100-100/HZ1-90-100A

QRS11-00100-100 (Standard)
QRS11-00100-101(Hi-Performance)

각속도 Full Range: ±100°/sec
Input 전압: ±5Vdc ±3%:
Full Scale Output: ±2.5VDc
Non-Linearity: ≤0.05% FS
사용온도: -40°C ~ +80°C

QRS14-0xxxx-102,  InVolt: +9~18V
          Full Scale Output: +1~4Vdc
QRS14-0xxxx-103,  InVolt: ±9~18V
          Full Scale Output: ±5Vdc

각속도: ±50, 100, 200, 500°/sec
Non-Linearity: ≤0.05% of FR
사용온도: -40°C ~ +85°C

HZ1-100-100  각속도: ±100°/sec
HZ1-90-100A  각속도: ±90°/sec

Input 전압: +9 ~ +15VDC
Full Scale Output: 0.5 ~ 4.5VDc
Non-Linearity: ≤0.05% of FR
사용온도: -40°C ~ +71°C

Applications:
    Stabilization
    Control
    Guidance
    Navigation

Applications:
    Platform/Camera Stabilization
    Riobotics, Instrumentation
    Short Term Navigation
    GPS Augmentation,
    Autonomous Vehicle Control

Applications:
    Antenna Stabilization Systems
    FA, Instrumentation
    Medical/Orthopedic
    GPS Augmentation, Navigation
    Vehicle Location System

SDG500-00100-100

SDG1000-200-100

QDARS     2축

MEMS Angular Rate Sensor

각속도 Full Range: ±100°/sec
Input 전압: ±5Vdc
Full Scale Output: ±5.0VDc
Non-Linearity: ≤0.05% FS
사용온도: -40°C ~ +85°C

MEMS Angular Rate Sensor

각속도 Full Range: ±200°/sec
Input 전압: ±10~16Vdc
Full Scale Output: ±5.0VDc
Non-Linearity: ≤0.03% FS
사용온도: -40°C ~ +85°C

Quartz Dual Axis Rate Sensor

각속도 Full Scale:  200°/sec
Input 전압: ±4.75 ~ ±5.35Vdc
Full Scale Output: ±3.50Vdc
Scale Factor: 17.5mV/°/sec
Scale Factor Accuracy: ±2%
Linearity Error: 0.05% of FS
사용온도: -55°C ~ +85°C

Applications:
 Small Business &
     Regional Aircraft
 Platform Stabilization
 Instrumentation
 Antennas and Pointing
 Motion Control
 Robotics and Robotic Vehicles
 

Applications:
  Primry/Secondry Stdby Attitude
        Indicators Systems
  Platform Stabilization
  Precise Instrumentation
  Short-Term Navigation
  Attitude & Heading Ref. Systems
  Aircraft Flight Control
  Robotics & Auto Vehicle Control

Applications:
  Radar/MissileSeekerHead/
    Gun/Optical sight Stabilization
  Autopilot/Guidance/Control
  Torpedo Attitude Control
   Fast Slewing Low Noise
     Scanning System

Angular Rate:    ±100°/sec
Acceleration:    ±1, 2, 5, 10 g's
Input 전압: ±15Vdc ±10%
              <270mA (each supply)
Full Scale Output, Rate: ±2.5Vdc
                        Accel: ±7.5Vdc
Non-Linearity, Rate: ≤0.05% FS
                    Accel: <50ug/g²
사용온도: -40°C ~ +80°C

Input 전압: ±15Vdc :  Mode 1
Angular Rate:    ±75°/sec
Acceleration:    ±1.5 g's
Hi Anlog Output: ±10Vdc
Lo Anlog Output: +0.5~+4.5Vdc
Non-Linearity, Rate: <3%
                    Accel: ±40mg
RS-232 Data Transfer Rate: 32Hz
사용온도: -40°C ~ +85°C

Input 전압: +12Vdc :  Mode 2
      Angular Rate:    ±75°/sec
       Acceleration:    ±1.5 g's

 Lo Anlog Output: +0.5~+4.5Vdc
      Non-Linearity, Rate: <3%
                       Accel: ±40mg
RS-232 Data Transfer Rate: 32Hz
         사용온도: -40°C ~ +85°C

Applications:
    Vehicle Instrumentation
    Robotics, Flight Testing
    Attitude Reference Systems
    Control Systems
    Dead Reckoning Aiding GPS
    Buoy Instrumentation

Features:
    Dual/Single Power Supply Opt.
    Dual Level Analog Outputs
    Digital (RS-232) Output
    Internal Temperature Sensor
    Long Operating Life
    Fully Self-Contained System
    Compact, Rugged Package

Applications:                          
    Vehicle Instrumentation
    Robotics, Flight Testing
    Remoptely Piloted Vehiclea
    Attitude Reference Systems
    Industrial Control Systems
    Navigation Aiding GPS
    Marine Instrumentation

INERTIAL MEASUREMENT UNITS

Inertial Navigation System/GPS System

Angular Rate:    200°/sec
Acceleration:    ±10 g
Input 전압: ±12Vdc @<5watt total
I/O :   RS-232            
ScaleFactor, Rate: .01°/sec/count
Scale Factor Error: <5000ppm
사용온도: -54°C ~ +70°C

Features:
    Δθ, ΔV Output at 100 Hz
    Linear Accel: Angular Rates
                        @600 Hz
    High-Vibration Environments
    High Performance Solution
    Small, Lightweight Design

Features:
    Optimized 28-state Kalman
      Filtered Navigation Solution
    High-Vibration Environments
    Integrated INS/GPS Solution
    Small, Lightweight Design
    Programmable Output

Features:
    Extremely Small Size
    Optimized 28-state Kalman
      Filtered Navigation Solution
    Integrated INS/GPS Solution
    RS-232 Digital Interface
    Accepts Data of Ext.        Magnetomer

Applications:
    Vehicle Instrumentation
    Robotics, Flight Testing
    Remoptely Piloted Vehiclea
    Attitude Reference Systems
    Industrial Control Systems
    Navigation Aiding GPS
    Marine Instrumentation

Applications:
    Position Sensor for
       Geo-Surveying    
    UAVs and Unmanned Vehicles
    Ground Vehicle Tracking
    Attitude Reference
    Precision Antenna Pointing
    Targeting and Positioning
    Range Instrumentation

Applications:
    Position Sensor for
       Geo-Surveying    
    UAVs and Unmanned Vehicles
    Ground Vehicle Tracking
    Attitude Reference
    Precision Antenna Pointing
    Targeting and Positioning
    Range Instrumentation

Applications:
    Position and Orientation System
      Stabulization    
    UAVs and Unmanned Veicles
    Tactical Missile/Smart Bombs
    Commercial Aviation/Rail Roads
    Long-Haul Commercial Transport.
    Targets and Drones/Helicopters
    Range Instrumentation