Beispiel #1
0
// read solution status -----------------------------------------------------
void __fastcall TPlot::ReadSolStat(TStrings *files, int sel)
{
    AnsiString s;
    gtime_t ts,te;
    double tint;
    int i,n=0;
    char *paths[MAXNFILE],id[32];
    
    trace(3,"ReadSolStat\n");
    
    freesolstatbuf(SolStat+sel);
    
    for (i=0;i<MAXNFILE;i++) paths[i]=path_str[i];
    
    TimeSpan(&ts,&te,&tint);
    
    for (i=0;i<files->Count&&n<MAXNFILE;i++) {
        strcpy(paths[n++],U2A(files->Strings[i]).c_str());
    }
    ShowMsg(s.sprintf("reading %s...",paths[0]));
    ShowLegend(NULL);
    
    readsolstatt(paths,n,ts,te,tint,SolStat+sel);
    
    UpdateSatList();
}
Beispiel #2
0
// update observation data index, azimuth/elevation, satellite list ---------
void __fastcall TPlot::UpdateObs(int nobs)
{
    AnsiString s;
    prcopt_t opt=prcopt_default;
    gtime_t time;
    sol_t sol={0};
    double pos[3],rr[3],e[3],azel[MAXOBS*2]={0},rs[6],dts[2],var;
    int i,j,k,svh,per,per_=-1;
    char msg[128];
    
    trace(3,"UpdateObs\n");
    
    delete [] IndexObs; IndexObs=NULL;
    delete [] Az; Az=NULL;
    delete [] El; El=NULL;
    NObs=0;
    if (nobs<=0) return;
    
    IndexObs=new int[nobs];
    Az=new double[Obs.n];
    El=new double[Obs.n];
    
    opt.err[0]=900.0;
    
    ReadWaitStart();
    ShowLegend(NULL);
    
    for (i=0;i<Obs.n;i=j) {
        time=Obs.data[i].time;
        for (j=i;j<Obs.n;j++) {
            if (timediff(Obs.data[j].time,time)>TTOL) break;
        }
        IndexObs[NObs++]=i;
        
        if (Nav.n<=0&&Nav.ng<=0&&Nav.ns<=0) {
            for (k=0;k<j-i;k++) Az[i+k]=El[i+k]=0.0;
            continue;
        }
        if (RcvPos==0) {
            pntpos(Obs.data+i,j-i,&Nav,&opt,&sol,azel,NULL,msg);
        }
        else {
            if (RcvPos==1) { // lat/lon/height
                for (k=0;k<3;k++) pos[k]=OOPos[k];
                pos2ecef(pos,rr);
            }
            else { // rinex header position
                for (k=0;k<3;k++) rr[k]=Sta.pos[k];
                ecef2pos(rr,pos);
            }
            for (k=0;k<j-i;k++) {
                azel[k*2]=azel[1+k*2]=0.0;
                if (!satpos(time,time,Obs.data[i+k].sat,EPHOPT_BRDC,&Nav,rs,dts,
                            &var,&svh)) continue;
                if (geodist(rs,rr,e)>0.0) satazel(pos,e,azel+k*2);
            }
        }
        for (k=0;k<j-i;k++) {
            Az[i+k]=azel[  k*2];
            El[i+k]=azel[1+k*2];
            if (Az[i+k]<0.0) Az[i+k]+=2.0*PI;
        }
        per=(i+1)*100/Obs.n;
        if (per!=per_) {
            ShowMsg(s.sprintf("updating azimuth/elevation... (%d%%)",(per_=per)));
            Application->ProcessMessages();
        }
    }
    IndexObs[NObs]=Obs.n;
    
    UpdateSatList();
    
    ReadWaitEnd();
}