File: StrapdownDownload  >Add to favorates  [Vote: very good!  5  4  3  2  1 Vote: very bad!]
  Directory: matlab
  Dev tools: matlab
  File size: 392 KB
  Update: 2010-06-02
  Downloads: 308
  Uploader: Ԭƽ
 Describe: First, data on: 1: inertial navigation system that links the north bit of the Czech system. Initial longitude 116.344695283 degrees latitude 39.975172, height h is 30 meters. Initial speed of v0 = [0.000048637 0.000206947 0.007106781], the same altitude. 2: jlfw for 600 seconds of data, gyroscopes and accelerometers were sampling period of 1/80 sec and 1/80 seconds. 3: Initial attitude angle [0.120992605 0.010445947 91.637207] (pitch, roll, heading, in units of degrees), jlfw than the power saved information f_INSc (unit m/s ^ 2), angular rate gyro information wib_INSc (units of rad/s), in the order of 1 ~ three lines were east, north, days to the information. 4: The heading angle is positive counterclockwise. 5: Earth ellipsoid long radius re = 6378245 Earth s rotation angular velocity wie = 7.292115147e-5 acceleration due to gravity g = g0* (1+ gk1* c33 ^ 2)* (1-2* h/re)/sqrt (1-gk2* c33 ^ 2) g0 = 9.7803267714 gk1 = 0.00193185138639 gk2 = 0.00669437999013
File list(Click to check if it's the file you need, and recomment it at the bottom):
  Strapdown
  .........\A2T.m
  .........\AVP_Calc.m
  .........\Calc_Initial.m
  .........\Data_Genetate.m
  .........\Delete_Bias.m
  .........\GetDataFromFile.m
  .........\GetParams.m
  .........\jl.dat
  .........\jl.ini
  .........\main.m
  .........\Oula_Angla.m
  .........\Para_Loading.m
  .........\Para_Setting.m
  .........\plot2.asv
  .........\plot2.m
  .........\PlotModeSetting.m
  .........\PlotResult.m
  .........\Q2T.m
  .........\Qone.m
  .........\Q_update.m
  .........\SkewMatrix_4.m
  .........\T2A.m
  .........\T2Q.m
  .........\V2AG.m
  .........\XwXa.mat
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