1362 bGetDouble(  in bGetDouble()  function
1387 #define bGetDouble(bp)        (*(double*)(bp))  macro
1494           if (bGetDouble(&buf[3]) != 0.0) {  in parse0x8FAD()
1617           tow =  bGetDouble(&buf[3]);  in parse0x8F0B()
1638           bias =              bGetDouble(&buf[18]) / GPS_C * 1e9;     /* ns */  in parse0x8F0B()
1639           rate =              bGetDouble(&buf[26]) / GPS_C * 1e9;     /* ppb */   in parse0x8F0B()
1642           lat =               bGetDouble(&buf[42]) * R2D;  in parse0x8F0B()
1643           lon =               bGetDouble(&buf[50]) * R2D;  in parse0x8F0B()
1644           alt =               bGetDouble(&buf[58]);  in parse0x8F0B()
1746           a0 = bGetDouble (buf);  in parse0x4F()
2339           *a0 = bGetDouble (buf);  in rpt_0x4F()
2522                               utcinfo->A_0       = bGetDouble (&buf4[13]);  in rpt_0x58()
2558                               navinfo->ephorb.M_0 = bGetDouble (&buf4[47]);  in rpt_0x58()
2560                               navinfo->ephorb.e = bGetDouble (&buf4[59]);  in rpt_0x58()
2562                               navinfo->ephorb.sqrt_A = bGetDouble (&buf4[71]);  in rpt_0x58()
2565                               navinfo->ephorb.OMEGA_0 = bGetDouble (&buf4[87]);  in rpt_0x58()
2567                               navinfo->ephorb.i_0 = bGetDouble (&buf4[99]);  in rpt_0x58()
2569                               navinfo->ephorb.omega = bGetDouble (&buf4[111]);  in rpt_0x58()
2572                               navinfo->ephorb.Axis = bGetDouble (&buf4[127]);  in rpt_0x58()
2573                               navinfo->ephorb.n = bGetDouble (&buf4[135]);  in rpt_0x58()
2574                               navinfo->ephorb.r1me2 = bGetDouble (&buf4[143]);  in rpt_0x58()
2575                               navinfo->ephorb.OMEGA_n=bGetDouble (&buf4[151]);  in rpt_0x58()
2576                               navinfo->ephorb.ODOT_n = bGetDouble (&buf4[159]);  in rpt_0x58()
2623           *time_of_fix = bGetDouble (&buf[17]);  in rpt_0x5A()
2758           ECEF_pos[0] = bGetDouble (buf);  in rpt_0x83()
2759           ECEF_pos[1] = bGetDouble (&buf[8]);  in rpt_0x83()
2760           ECEF_pos[2] = bGetDouble (&buf[16]);  in rpt_0x83()
2761           *clock_bias  = bGetDouble (&buf[24]);  in rpt_0x83()
2781           *lat = bGetDouble (buf);  in rpt_0x84()
2782           *lon = bGetDouble (&buf[8]);  in rpt_0x84()
2783           *alt = bGetDouble (&buf[16]);  in rpt_0x84()
2784           *clock_bias = bGetDouble (&buf[24]);  in rpt_0x84()
2874           *tow = bGetDouble(&buf[3]);  in rpt_0x8F0B()
2880           *bias = bGetDouble(&buf[18]);  in rpt_0x8F0B()
2881           *drift = bGetDouble(&buf[26]);  in rpt_0x8F0B()
2884           *lat = bGetDouble(&buf[42]);  in rpt_0x8F0B()
2885           *lon = bGetDouble(&buf[50]);  in rpt_0x8F0B()
2886           *alt = bGetDouble(&buf[58]);  in rpt_0x8F0B()
2905           datum_coeffs[0] = bGetDouble (&buf[3]);  in rpt_0x8F14()
2906           datum_coeffs[1] = bGetDouble (&buf[11]);  in rpt_0x8F14()
2907           datum_coeffs[2] = bGetDouble (&buf[19]);  in rpt_0x8F14()
2908           datum_coeffs[3] = bGetDouble (&buf[27]);  in rpt_0x8F14()
2909           datum_coeffs[4] = bGetDouble (&buf[35]);  in rpt_0x8F14()
2927           datum_coeffs[0] = bGetDouble (&buf[3]);  in rpt_0x8F15()
2928           datum_coeffs[1] = bGetDouble (&buf[11]);  in rpt_0x8F15()
2929           datum_coeffs[2] = bGetDouble (&buf[19]);  in rpt_0x8F15()
2930           datum_coeffs[3] = bGetDouble (&buf[27]);  in rpt_0x8F15()
2931           datum_coeffs[4] = bGetDouble (&buf[35]);  in rpt_0x8F15()
3081           *pps_offset = bGetDouble(&buf[4]);  in rpt_0x8F4A_16()
3152           *FracSec = bGetDouble(&rpt->buf[3]);  in rpt_0x8FAD()