Under the condition of high dynamic angular motion or vibration environment, confirmed and corrected the sculling error is important to calculated the speed of strap-down inertial navigation system.
With regard to the scheme of inertial navigation system correction with airborne radar, this paper studies the radar performance requirement in order to meet the correction precision.
This area of study is central to the technology of inertial navigation and gyroscopic stabilization.
minimal ship's inertial navigation system
An online identification algorithm of odometer's scale factor in land used strapdown inertial navigation system is put forward.
In the thesis, the technology of initial alignment and transfer alignment of the inertial navigation system of the carrier borne plane when the aircraft carrier is moored or is cruising is researched.
A inertial navigation system, this module includes forward back pluse signals, the gyro signal, speed pulse signal and the barometer signal.
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