Sell Innalabs AHRS

Description

Innalabs©AHRS (Attitude Heading Reference System) is a high performance strapdown system that determines full angular orientation of any vehicle or other carrier in 3D space. Main Applications Land Vehicle Control Remotely Operated Vehicles Avionics System Platform Stabilization Robotics FEATURES Real‐Time Precision Roll, Pitch and Heading angle in dynamic environment 3‐Axis Inertial Outputs Fully Compensated Over Wide Temperature Range Small Dimension Low power Low weight EMI & Vibration Resistant Environmentally Sealed RS‐**2 Serial Outputs (USB outputs are optional) Performance Update Rate (Hz) 1…..**0 (user settable) Start-up Time (sec) < 1 Full Accuracy Data (Warm-up Time) (sec) < *0 Heading Range (deg) 0 to **0 Static Accuracy at Normal Conditions (Tc=*5°C) (deg RMS) 0, 2 Static Accuracy in Temperature Range (Tc=**0°C to **0°C) (deg RMS) 0, 5 Dynamic Accuracy (deg RMS) 0, 7 Noise (at **0Hz output, deg RMS) 0.*2 Resolution (deg) 0.*1 Attitude Range: Pitch, Roll (deg) ±*0, ±**0 Static Accuracy at Normal Conditions (Tc=*5°C) (deg RMS) 0, *4 Static Accuracy in Temperature Range (Tc=**0°C to **0°C) (deg RMS) 0, 1 Dynamic Accuracy (deg RMS) 0, 4 Noise (at **0Hz output, deg RMS) 0.*2 Resolution (deg) 0.*1 Angular Rate Input Range: Yaw, Pitch, Roll (deg/sec) ±**0 Bias (deg/sec RMS) 0, *2 Scale Factor Accuracy (%) 0, 2 Non-Linearity (% FS) 0, 1 Random Walk (deg/sqrt(hr)) 6 Resolution (deg/sec) 0, *1 Bandwidth (Hz) *0 Linear acceleration Input Range: X/Y/Z (g) ±2 Bias (mg RMS) 0, 3 Scale Factor Accuracy (%) < 0.1 Non-Linearity (% FS) 0, 2 Random Walk (m/s/sqrt(hour)) 0, *6 Resolution (mg) < *0 Bandwidth (Hz) *0 Environment Operating Temperature (deg C) – *0 to **0 Non-Operating Temperature (deg C) – *5 to **5 Electrical Input Voltage (VDC) *5.5 to *6.5 Input Current (mA) < **0