RTKLIB专题学习(七)—精密单点定位实现初识(二)
上一节我们讲完了pppos中状态的时间更新函数的内容了,接下来我们往下进行:
1.satposs是pppps调用的另一个函数,主要用于计算卫星位置rs和卫星钟差dts
/* satellite positions and clocks ----------------------------------------------
* compute satellite positions, velocities and clocks
* args : gtime_t teph I time to select ephemeris (gpst)
* obsd_t *obs I observation data
* int n I number of observation data
* nav_t *nav I navigation data
* int ephopt I ephemeris option (EPHOPT_???)
* double *rs O satellite positions and velocities (ecef)
* double *dts O satellite clocks
* double *var O sat position and clock error variances (m^2)
* int *svh O sat health flag (-1:correction not available)
* return : none
* notes : rs [(0:2)+i*6]= obs[i] sat position {x,y,z} (m)
* rs [(3:5)+i*6]= obs[i] sat velocity {vx,vy,vz} (m/s)
* dts[(0:1)+i*2]= obs[i] sat clock {bias,drift} (s|s/s)
* var[i] = obs[i] sat position and clock error variance (m^2)
* svh[i] = obs[i] sat health flag
* if no navigation data, set 0 to rs[], dts[], var[] and svh[]
* satellite position and clock are values at signal transmission time
* satellite position is referenced to antenna phase center
* satellite clock does not include code bias correction (tgd or bgd)
* any pseudorange and broadcast ephemeris are always needed to get
* signal transmission time
*-----------------------------------------------------------------------------*/
extern void satposs(gtime_t teph, const obsd_t *obs, int n, const nav_t *nav,
int ephopt, double *rs, double *dts, double *var, int *svh)
{
gtime_t time[2*MAXOBS]={
{
0}};
double dt,pr;
int i,j;
trace(3,"satposs : teph=%s n=%d ephopt=%d\n",time_str(teph,3),n,ephopt);
for (i=0;i<n&&i<2*MAXOBS;i++) {
for (j=0;j<6;j++) rs [j+i*6]=0.0;
for (j=0;j<2;j++) dts[j+i*2]=0.0;
var[i]=0.0; svh[i]=0;
/* search any pseudorange */
for (j=0,pr=0.0;j<NFREQ;j++) if ((pr=obs[i].P[j])!=0.0) break;
if (j>=NFREQ) {
trace(3,"no pseudorange %s sat=%2d\n",time_str(obs[i].time,3),obs[i].sat);
continue;
}
/* transmission time by satellite clock */
time[i]=timeadd(obs[i].time,-pr/CLIGHT);
/* satellite clock bias by broadcast ephemeris */
if (!ephclk(time[i],teph,obs[i].sat,nav,&dt)) {
trace(3,"no broadcast clock %s sat=%2d\n",time_str(time[i],3),obs[i].sat);
continue;
}
time[i]=timeadd(time[i],-dt);
/* satellite position and clock at transmission time */
if (!satpos(time[i],teph,obs[i].sat,ephopt,nav,rs+i*6,dts+i*2,var+i,
svh+i)) {
trace(3,"no ephemeris %s sat=%2d\n",time_str(time[i],3),obs[i].sat);
continue;
}
/* if no precise clock available, use broadcast clock instead */
if (dts[i*2]==0.0) {
if (!ephclk(time[i],teph,obs[i].sat,nav,dts+i*2)) continue;
dts[1+i*2]=0.0;
*var=SQR(STD_BRDCCLK);
}
}
for (i=0;i<n&&i<2*MAXOBS;i++) {
trace(4,"%s sat=%2d rs=%13.3f %13.3f %13.3f dts=%12.3f var=%7.3f svh=%02X\n",
time_str(time[i],6),obs[i].sat,rs[i*6],rs[1+i*6],rs[2+i*6],
dts[i*2]*1E9,var[i],svh[i]);
}
}
2.tidedisp是pppos调用的又一个函数,用于计算固体潮
海洋潮汐以及极潮对接收机位置产生的影响
/* tidal displacement ----------------------------------------------------------
* displacements by earth tides
* args : gtime_t tutc I time in utc
* double *rr I site position (ecef) (m)
* int opt I options (or of the followings)
* 1: solid earth tide
* 2: ocean tide loading
* 4: pole tide
* 8: elimate permanent deformation
* double *erp I earth rotation parameters (NULL: not used)
* double *odisp I ocean loading parameters (NULL: not used)
* odisp[0+i*6]: consituent i amplitude radial(m)
* odisp[1+i*6]: consituent i amplitude west (m)
* odisp[2+i*6]: consituent i amplitude south (m)
* odisp[3+i*6]: consituent i phase radial (deg)
* odisp[4+i*6]: consituent i phase west (deg)
* odisp[5+i*6]: consituent i phase south (deg)
* (i=0:M2,1:S2,2:N2,3:K2,4:K1,5:O1,6:P1,7:Q1,
* 8:Mf,9:Mm,10:Ssa)
* double *dr O displacement by earth tides (ecef) (m)
* return : none
* notes : see ref [1], [2] chap 7
* see ref [4] 5.2.1, 5.2.2, 5.2.3
* ver.2.4.0 does not use ocean loading and pole tide corrections
*-----------------------------------------------------------------------------*/
extern void tidedisp(gtime_t tutc, const double *rr, int opt, const erp_t *erp,
const double *odisp, double *dr)
{
gtime_t tut;
double pos[2],E[9],drt[3],denu[3],rs[3],rm[3],gmst,erpv[5]={
0};
int i;
#ifdef IERS_MODEL
double ep[6],fhr;
int year,mon,day;
#endif
trace(3,"tidedisp: tutc=%s\n",time_str(tutc,0));
if (erp) {
geterp(erp,utc2gpst(tutc),erpv);
}
tut=timeadd(tutc,erpv[2]);
dr[0]=dr[1]=dr[2]=0.0;
if (norm(rr,3)<=0.0) return;
pos[0]=asin(rr[2]/norm(rr,3));
pos[1]=atan2(rr[1],rr[0]);
xyz2enu(pos,E);
if (opt&1) {
/* solid earth tides */
/* sun and moon position in ecef */
sunmoonpos(tutc,erpv,rs,rm,&gmst);
#ifdef IERS_MODEL
time2epoch(tutc,ep);
year=(int)ep[0];
mon =(int)ep[1];
day =(int)ep[2];
fhr =ep[3]+ep[4]/60.0+ep[5]/3600.0;
/* call DEHANTTIDEINEL */
dehanttideinel_((double *)rr,&year,&mon,&day,&fhr,rs,rm,drt);
#else
tide_solid(rs,rm,pos,E,gmst,opt,drt);
#endif
for (i=0;i<3;i++) dr[i]+=drt[i];
}
if ((opt&2)&&odisp) {
/* ocean tide loading */
tide_oload(tut,odisp,denu);
matmul("TN",3,1,3

本文详细介绍了RTKLIB中精密单点定位的实现过程,包括计算卫星位置、钟差、固体潮汐影响、相位和码残差以及扩展卡尔曼滤波。通过pppos、tidedisp、ppp_res和filter等函数,实现了从观测数据到解算接收机位置的过程。在解算后,进行后验残差分析,符合要求则输出为精密单点定位状态。
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