ignav configuration
ignav中的坐标系
n-frame:n-e-d
b-frame:f-r-d
stats-eratio1 =100
stats-eratio2 =100
stats-errphase =0.003 # (m) 高度角随机模型 :a*a+b*b/(sinel*sinel*)中的a,论文中说a=0.004m
stats-errphaseel =0.003 # (m) 高度角随机模型 :a*a+b*b/(sinel*sinel*)中的b,论文中说b=0.003m
stats-errphasebl =0 # (m/10km)
stats-errdoppler =10 # (Hz)
stats-stdbias =30 # (m)
stats-stdiono =0.03 # (m)
stats-stdtrop =0.3 # (m)
stats-prnaccelh =10 # (m/s^2)
stats-prnaccelv =10 # (m/s^2)
stats-prnbias =0.0001 # (m)
stats-prniono =0.001 # (m)
stats-prntrop =0.0001 # (m)
stats-clkstab =5e-12 # (s/s)
ins-leverarm1 = 0.0 # lever arm from INS to GPS antenna in frd-frame (pos-gnss = pos-ins + Cbe*L^b )
ins-leverarm2 = 0.153
ins-leverarm3 =-0.179
ins-imuformat =2 # imu measurement data format
ins-imudecfmt =1 # imu measurement decode format (1: angular rate/acceleration, 2:angular/velocity increment)
ins-imucoors =2 # imu body coordinate frame(1:前右下,2:右前上)
ins-imuvalfmt =1 # imu measurement gyro data value format(1:degree, 2:rad)
ins-exprn =0 # use extend method to get process noise matrix
ins-exphi =0 # use precise system propagate matrix for ekf
ins-exvm =0 # extend method to velocity matching for ins navigation initial
ins-iisu =2 # initial ins state use rtk options (SOLQ_???)
ins-nhc =0 # non-holonomic constraint options (0:off,1:on)
ins-zvu =0 # zero velocity update options (0:off,1:on)
ins-zaru =0 # zero augular rate update options (0:off,1:on)
ins-detst =0 # detect static imu measurement data (0:off,1:on)
ins-tc =4 # ins-gnss tightly coupled mode (INSTC_???)---------------------------1.single point position 2.PPP-kinematic 3.DGPS 4.RTK
ins-lc = # ins-gnss loosely coupled mode (INSLC_???)
ins-doppler = # use doppler measurement to aid ins updates states
ins-intpref =
ins-minp =
ins-hz =200.0 # imu measurement sampling frequency
ins-nhz =100.0 # non-holonomic constraint update frequency
ins-lcopt =3 # ins-gnss loosely coupled use gnss observation or gsof message-----1.gsof message data 2.code/phase observation data 3.pvt solution data
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