Testing of Electronic Stability Control systems and airbag sensors. The systems may be use as many as two rate gyros and one accelerometer.
To Use in universities and research laboratories for development of inertial sensors, their performance levels, and lower-cost and smaller sensors.
Simulators are intended for use during development, production, in-process testing, calibration and final inspection of MEMS sensors.
Attitude and orbital control Systems components, such as optoelectronic equipment (e.g. star trackers, sun sensors), test and calibrate by simulators.
Simulation in Hardware-In-the-Loop during development programs can help reduce time and cost, by minimizing the number of field trials required.
Testing and calibration of Inertial Navigation Systems (INS) that are installed on board commercial airliners, jet airplanes, and helicopters.
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