Alignment method with combination of strap-down inertial navigation and tachometer based on reverse navigation algorithm
A strapdown inertial navigation and navigation algorithm technology, applied in the field of inertial navigation alignment, can solve the problems of expensive DVL, inability to guarantee measurement accuracy, exposure, etc.
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[0102] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:
[0103] Step 1: Build the SINS and tachometer alignment model:
[0104] Transition equation:
[0105] Observation equation: Z ST =H ST x ST +v ST
[0106] In the above formula
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[0113] Among them, F ST is the system state matrix, H ST is the system measurement matrix, the system noise w ST and measurement noise μ ST It is white Gaussian noise with zero mean. V N , V U , V E is the speed of the carrier in the north sky direction, λ, L and h represent the longitude, latitude and height of the carrier respectively, and the height information can be directly measured by the depth sensor.
[0114] Establish the differential equation of the forward navigation algorithm and discretize it:
[0115] Attitude equation:
[0116] Velocity equation:
[0117] Position equation:
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