Test Case 1: Creating an empty CC object and loading the data.
Clock Correction co1: 0.00072319419646

Test Case 2: Creating CC object with data.
ClockCorrection co2: 0.00072319419646

Test Case 3: Creating CC object with raw legacy nav message data.
Clock Correction co3: 0.00072319419678

Test Case 4: Creating CC object with raw legacy nav message data.
Clock Correction co4: 0.00072319419678

Test Case 5: Creating CC object with data from RINEX file.
Clock Correction co5: 0.00072319419678

Test Case 6: Calculated clock correction using 'classic' EngEphemeris.
Time= 06/02/2011 12:14:44 GPS
Clock Bias EE:  0.00072319419678
Clock Drift EE: 5.1159076975e-12

Test Case 7: Calculated clock corrections using 'classic' EngEphemeris.
Time = 06/04/2011 11:30:00 GPS
Clock Bias EE:  8.4248039457e-05
Clock Drift EE: 2.3874235922e-12

Test Case 8: Calculated clock corrections using 'classic' EngEphemeris.
Time = 06/05/2011 01:00:00 GPS
Clock Bias EE:  8.4364068243e-05
Clock Drift EE: 2.3874235922e-12

Dump Output for Test Cases 4 and 6.
dump EE:
****************************************************************************
Broadcast Ephemeris (Engineering Units) -FIC

PRN :  3

              Week(10bt)     SOW     DOW   UTD     SOD   MM/DD/YYYY   HH:MM:SS
Clock Epoch:  1638( 614)  388800   Thu-4   153   43200   06/02/2011   12:00:00
Eph Epoch:    1638( 614)  388800   Thu-4   153   43200   06/02/2011   12:00:00
Transmit Time:1638( 614)  381600   Thu-4   153   36000   06/02/2011   10:00:00
Fit interval flag :  0

          SUBFRAME OVERHEAD

               SOW    DOW:HH:MM:SS     IOD    ALERT   A-S
SF1 HOW:    381606  Thu-4:10:00:06   0x016      0      on
SF2 HOW:    381612  Thu-4:10:00:12    0x16      0      on
SF3 HOW:    381618  Thu-4:10:00:18    0x16      0      on

           CLOCK

Bias T0:       7.23189674E-04 sec
Drift:         5.11590770E-12 sec/sec
Drift rate:    0.00000000E+00 sec/(sec**2)
Group delay:  -4.65661287E-09 sec

           ORBIT PARAMETERS

Semi-major axis:         5.15365528E+03 m**.5
Motion correction:       5.39093884E-09 rad/sec
Eccentricity:            1.42575260E-02
Arg of perigee:          1.09154605E+00 rad
Mean anomaly at epoch:   1.05539163E+00 rad
Right ascension:        -2.16947563E+00 rad     -8.56285668E-09 rad/sec
Inclination:             9.28692498E-01 rad      5.52880173E-10 rad/sec

           HARMONIC CORRECTIONS

Radial        Sine:   1.87812500E+01 m    Cosine:   2.03562500E+02 m
Inclination   Sine:   5.02914190E-08 rad  Cosine:  -2.30967999E-07 rad
In-track      Sine:   8.35768878E-06 rad  Cosine:   9.57399607E-07 rad

           SV STATUS

Health bits:   0x00      URA index:    0
Code on L2:    P only    L2 P Nav data:          on

dump co4:
****************************************************************************
Broadcast Ephemeris (Engineering Units)

PRN :  3

              Week(10bt)     SOW     DOW   UTD     SOD  MM/DD/YYYY   HH:MM:SS
Clock Epoch:  1638( 614)  388800   Thu-4   153   43200  06/02/2011   12:00:00

           CLOCK

Bias T0:      7.23189674318E-04 sec
Drift:        5.11590769747E-12 sec/sec
Drift rate:   0.00000000000E+00 sec/(sec**2)
****************************************************************************

