Description: Strapdown inertial navigation system, using the quaternion method the state variables estimated ~ and applied to the SINS/GPS Integrated Navigation System ~
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File list (Check if you may need any files):
SINS
....\a2caw.m
....\a2cnb.m
....\a2cwa.m
....\a2qnb.m
....\askew.m
....\cnscl.m
....\earth.m
....\getf.m
....\glvs.m
....\kalman.m
....\kfdis.m
....\m2att.m
....\m2qnb.m
....\q2att.m
....\q2cnb.m
....\q2rv.m
....\qaddphi.m
....\qconj.m
....\qdelphi.m
....\qmul.m
....\qmulv.m
....\qq2phi.m
....\readme.txt
....\rv2q.m
....\sins.m
....\test_align_compass.asv
....\test_align_compass.m
....\test_align_kalman.m
....\test_cone_error.m
....\test_cone_gen.m
....\test_cone_gen_1deg_1Hz.mat
....\test_sins.m
....\test_SINS_GPS.m
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