The present invention belongs to the field of navigation technology, and specifically relates to a Doppler
radar assisted strapdown inertial navigation motion base rough alignment method under large
azimuth misalignment angle. Step 1: define gyro constant drift and
accelerometer constant error, establish the coordinate
transformation matrix from ideal navigation coordinate
system n to actual navigation coordinate
system n′ and the mathematical platform attitude
error equation and velocity
error equation of strapdown inertial navigation under large
azimuth misalignment angle; Step 2: establish the state equation of strapdown inertial navigation motion base rough alignment under large
azimuth misalignment angle, and obtain the state matrix; Step 3: construct the measurement of
Doppler velocity radar assisted strapdown inertial navigation rough alignment, and then combine it with the coordinate
transformation matrix of step 1 to obtain the measurement equation and measurement matrix of strapdown inertial navigation motion base rough alignment under large azimuth misalignment angle; Step 4: use t k Measurement of time Z k The
Kalman filter is used to realize the rough alignment filtering solution of the strapdown
inertial navigation system moving base under large azimuth misalignment angle, thereby realizing the rough alignment of the strapdown
inertial navigation system.