exp1

说明：  捷联惯导系统放置在室内测试台上做静态测试，测试时间4500s。 1）取前180数据做粗对准（解析对准法）； 2）取第181s~900s数据做精对准（Kalman滤波法）； 3）从第901s开始做纯惯导解算； 4）用国军标的导航系统位置精度评价方法评估系统定位精度（分别计算CEP50 和 CEP95 下的定位精度）。(The strapdown inertial navigation system was placed on the indoor test bench for static test with a test time of 4500s. 1) take the first 180 data for rough alignment (analytical alignment method); 2) accurate alignment of 181s-900s data (Kalman filtering method); 3) pure inertial navigation solution is performed from 901s; 4) the positioning accuracy of the navigation system is evaluated by the method of position accuracy evaluation of the national military standard (the positioning accuracy under CEP50 and CEP95 are calculated respectively).)

exp1, 0 , 2018-07-28
exp1\coarse_align.m, 751 , 2018-07-07
exp1\dcm2eul.m, 274 , 2018-06-09
exp1\dcm2qua.m, 241 , 2018-06-09
exp1\eul2dcm.m, 489 , 2018-06-09
exp1\eul2qua.m, 439 , 2018-06-09
exp1\initpara.m, 389 , 2018-07-07
exp1\ins_navi.m, 1402 , 2018-07-27
exp1\KF_correct.m, 1552 , 2018-06-28
exp1\main.m, 2629 , 2018-07-27
exp1\pre_data.m, 584 , 2018-07-07
exp1\qua2dcm.m, 310 , 2018-06-09
exp1\qua_multiply.m, 225 , 2018-06-09