display.m

There are numerous MATLAB m-files included in this software package. Thus, the the authors have bund

function display(b)

% PRN / EPOCH / SV CLK
fprintf('Satellite PRN number               iPRN            : %4i\n',b.iPRN)
fprintf('Epoch year                         iEpochYear      : %4i\n',b.iEpochYear)
fprintf('Epoch month                        iEpochMonth     : %4i\n',b.iEpochMonth)
fprintf('Epoch day                          iEpochDay       : %4i\n',b.iEpochDay)
fprintf('Epoch hour                         iEpochHour      : %4i\n',b.iEpochHour)
fprintf('Epoch minute                       iEpochMinute    : %4i\n',b.iEpochMinute)
fprintf('Epoch second                       iEpochSecond    : %4i\n',b.iEpochSecond)
fprintf('Sat Clock Bias (sec)               dClockBias      : %6.8f\n',b.dClockBias)
fprintf('Sat Clock drift(sec/sec)           dClockDrift     : %6.8f\n',b.dClockDrift)
fprintf('Sat Clock drift rate (sec/sec2)    dClockDriftRate : %6.8f\n',b.dClockDriftRate)

% BROADCAST ORBIT - 1
fprintf('IDOE Issue of Data, Ephemeris      dIDOE   : %6.8f\n',b.dIDOE)
fprintf('Crs (meters)                       dCrs    : %6.8f\n',b.dCrs)
fprintf('Sat Clock drift rate (sec/sec2)    dM0     : %6.8f\n',b.dDeltaN)
fprintf('M0 (radians)                       dDeltaN : %6.8f\n',b.dM0)

% BROADCAST ORBIT - 2
fprintf('Cuc (radians)                      dCuc    : %6.8f\n',b.dCuc)
fprintf('e Eccenricity                      dEccent : %6.8f\n',b.dEccent)
fprintf('Cus (radians)                      dCus    : %6.8f\n',b.dCus)
fprintf('sqrt(A) (sqrt(m)                   dSqrtA  : %6.8f\n',b.dSqrtA)

% BROADCAST ORBIT - 3
fprintf('Toe Time of Ephemeris(sec of Week) dToe    : %6.8f\n',b.dToe)
fprintf('Cic (radians)                      dCic    : %6.8f\n',b.dCic)
fprintf('OMEGA (radians)                    dOMEGA  : %6.8f\n',b.dOMEGA)
fprintf('Cis (radians)                      dCis    : %6.8f\n',b.dCis)

% BROADCAST ORBIT - 4
fprintf('i0                                 di0      : %6.8f\n',b.di0)
fprintf('Crc (radians)                      dCrc     : %6.8f\n',b.dCrc)
fprintf('omega (radians)                    dOmega   : %6.8f\n',b.dOmega)
fprintf('OMEGA Dot (radians)                dOMEGADot: %6.8f\n',b.dOMEGADot)

% BROADCAST ORBIT - 5
fprintf('Idot                               dIdot       : %6.8f\n',b.dIdot)
fprintf('Codes on L2 channel                dCodeOnL2   : %6.8f\n',b.dCodeOnL2)
fprintf('GPS Week # (to go with TOE)        dGpsWeek    : %6.8f\n',b.dGpsWeek)
fprintf('L2 P data flag                     dPDataFlag  : %6.8f\n',b.dPDataFlag)

% BROADCAST ORBIT - 6   
fprintf('SV Accuracy (meters)               dSVaccur    : %6.8f\n',b.dSVaccur)
fprintf('SV health   (MSB only)             dSVhealth   : %6.8f\n',b.dSVhealth)
fprintf('TGD (seconds)                      dTGD        : %6.8f\n',b.dTGD)
fprintf('IODC Issue of Data, Clock          dIODC       : %6.8f\n',b.dIODC)

% BROADCAST ORBIT - 7
fprintf('Transmission time of message       dTransTime  : %6.8f\n',b.dTransTime)
fprintf('Spare 1                            dSpare1     : %6.8f\n',b.dSpare1)
fprintf('Spare 2                            dSpare2     : %6.8f\n',b.dSpare2)
fprintf('Spare 3                            dSpare3     : %6.8f\n',b.dSpare3)

b.dtStart
b.dtEnd