コード例 #1
0
ファイル: t_tle.c プロジェクト: HoughtonAssoc/rtklib-mops
/* tle_pos() accuracy --------------------------------------------------------*/
static void utest3(void)
{
    const char *file1="../data/tle/brdc3050.12*";
    const char *file2="../data/tle/TLE_GNSS_20121101.txt";
    const char *file3="../data/tle/igs17127.erp";
    const double ep[6]={2012,10,31,0,0,0};
    nav_t nav={0};
    erp_t erp={0};
    tle_t tle={0};
    gtime_t time;
    char sat[32];
    double rs1[6],rs2[6],ds[6],dts[2],var;
    int i,j,k,stat,svh;
    
    readrnx(file1,0,"",NULL,&nav,NULL);
        assert(nav.n>0);
    
    stat=readerp(file3,&erp);
        assert(stat);
    
    stat=tle_read(file2,&tle);
        assert(stat);
    
    for (i=0;i<MAXSAT;i++) {
        satno2id(i+1,sat);
        
        fprintf(OUT,"SAT=%s\n",sat);
        
        for (j=0;j<96;j++) {
            time=timeadd(epoch2time(ep),900.0*j);
            
            if (!satpos(time,time,i+1,EPHOPT_BRDC,&nav,rs1,dts,&var,&svh)) continue;
            
            if (satsys(i+1,NULL)==SYS_QZS) svh&=0xFE;
            
            if (svh) continue;
            
            stat=tle_pos(time,sat,"","",&tle,&erp,rs2);
                assert(stat);
            
            for (k=0;k<3;k++) ds[k]=rs2[k]-rs1[k];
            
            fprintf(OUT,"%6.0f %11.3f %11.3f %11.3f %11.3f\n",900.0*j,
                    ds[0]/1e3,ds[1]/1e3,ds[2]/1e3,norm(ds,3)/1e3);
                
                assert(norm(ds,3)/1e3<300.0);
        }
        fprintf(OUT,"\n");
    }
    fprintf(OUT,"%s utest3 : OK\n",__FILE__);
}
コード例 #2
0
ファイル: postpos.c プロジェクト: idaohang/rtk-streamserver
/* open procssing session ----------------------------------------------------*/
static int openses(const prcopt_t *popt, const solopt_t *sopt,
                   const filopt_t *fopt, nav_t *nav, pcvs_t *pcvs, pcvs_t *pcvr)
{
    char *ext;
    
    trace(3,"openses :\n");
    
    /* read satellite antenna parameters */
    if (*fopt->satantp&&!(readpcv(fopt->satantp,pcvs))) {
        showmsg("error : no sat ant pcv in %s",fopt->satantp);
        trace(1,"sat antenna pcv read error: %s\n",fopt->satantp);
        return 0;
    }
    /* read receiver antenna parameters */
    if (*fopt->rcvantp&&!(readpcv(fopt->rcvantp,pcvr))) {
        showmsg("error : no rec ant pcv in %s",fopt->rcvantp);
        trace(1,"rec antenna pcv read error: %s\n",fopt->rcvantp);
        return 0;
    }
    /* read dcb parameters */
    if (*fopt->dcb) {
        readdcb(fopt->dcb,nav);
    }
    /* read ionosphere data file */
    if (*fopt->iono&&(ext=strrchr(fopt->iono,'.'))) {
        if (strlen(ext)==4&&(ext[3]=='i'||ext[3]=='I')) {
            readtec(fopt->iono,nav,0);
        }
#ifdef EXTSTEC
        else if (!strcmp(ext,".stec")||!strcmp(ext,".STEC")) {
            stec_read(fopt->iono,nav);
        }
#endif
    }
    /* open geoid data */
    if (sopt->geoid>0&&*fopt->geoid) {
        if (!opengeoid(sopt->geoid,fopt->geoid)) {
            showmsg("error : no geoid data %s",fopt->geoid);
            trace(2,"no geoid data %s\n",fopt->geoid);
        }
    }
    /* read erp data */
    if (*fopt->eop) {
        if (!readerp(fopt->eop,&nav->erp)) {
            showmsg("error : no erp data %s",fopt->eop);
            trace(2,"no erp data %s\n",fopt->eop);
        }
    }
    return 1;
}