Method for performing rapid initial alignment on strapdown inertial navigation system of launched underwater vehicle
An inertial navigation system and underwater navigation technology, applied in the direction of instruments, measuring devices, etc., can solve problems such as difficulty in applying rapid initial alignment, achieve the effects of reducing launch preparation time, improving maneuverability, and reducing the duration of fine alignment
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[0111] The three-axis zero drift of the strapdown inertial navigation gyroscope installed on the underwater vehicle is 0.005 / h, and the three-axis zero offset of the accelerometer is 50 μg. Doppler velocity meter accuracy is 1% ± 1mm / s. The launch site is located at a latitude of 32.62°. The attitude angle (pitch angle, roll angle, azimuth angle) of the underwater vehicle before launch is [0° 0° 45°] T . After launch, it will carry out a constant speed and direct flight with a heading of 45° east by north and a speed of 10m / s. Set the alignment time to 300 seconds, ie t s = 0s, t e = 300s.
[0112] Step 1: The underwater vehicle is roughly aligned on the carrier platform to obtain a rough attitude array and initial velocity v n (t s0 ). by attitude array and the true value of aircraft attitude [0° 0° 45°] T Comparison, it can be obtained that the misalignment angle at this time is [10' 10' 120'] T . initial velocity v n (t s0 )=[7m / s 7m / s 0m / s] T .
[0113] ...
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