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WORING IN RESULT THE PROBLEM OF POINTER
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@@ -12,71 +12,9 @@
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#include"deg2dms.h"
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#include"blh2enu.h"
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#include"rahcal.h"
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/* -------------------------------------------------------------------------- */
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#define a 6378137.0//长半轴
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#define f (1 / 298.257223563)//扁率
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#define e2 (f*(2-f))//第一偏心率平方
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#define C_V 299792458//光速(m)
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#define GM 398600500000000//地心引力常数
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#define math_e 2.718281828459 //e值
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#define PI 3.141592653589793
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#define Earth_e 7.2921151467e-5 //地球自转角速度
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#define C1 0
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/* -------------------------------------------------------------------------- */
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//卫星位置结构体
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typedef struct
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{
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double X[36];
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double Y[36];
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double Z[36];
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double deltat[36];//改正前的信号传播时间
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double delta_t[36];//改正后的信号传播时间
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double delta_clk[36];
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}pos_t, *ppos_t;
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//测站位置结构体
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typedef struct
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{
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double X;
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double Y;
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double Z;
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double B;
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double L;
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double H;
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double delta_TR;
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}station, *pstation;
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typedef struct
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{
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double B;
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int B_d;
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int B_m;
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int B_s;
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double L;
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int L_d;
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int L_m;
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int L_s;
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double H;
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}blh, *pblh;
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typedef struct enu
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{
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double E;
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double N;
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double U;
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}enu, *penu;
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typedef struct rah
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{
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double R;
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double A;
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double H;
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}rah, *prah;
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/* ------------------------------- GPS卫星位置计算函数 ------------------------------ */
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int gps_pos(int eponum, int sPRN, int best_epoch, double GPSsec,
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/* ------------------------------- GPS卫星位置计算函数 ------------------------------ */
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int gps_pos(int eponum, int sPRN, int best_epoch, double GPSsec,
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pnav_body nav_b, pobs_head obs_h, ppos_t pos_t)
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{
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double T_S = GPSsec - pos_t[eponum].deltat[sPRN];//计算信号发射时刻
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@@ -120,15 +58,15 @@
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double rela = 2*sqrt(GM) * nav_b[best_epoch].e * nav_b[best_epoch].sqrtA * sin(Es)/pow(C_V,2);
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pos_t[eponum].delta_clk[sPRN] = nav_b[best_epoch].sa0 + nav_b[best_epoch].sa1 * tk + nav_b[best_epoch].sa2 * pow(tk,2) - rela;
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}
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/* -------------------------------------------------------------------------- */
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/* -------------------------------------------------------------------------- */
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/* ------------------------------- GPS卫星位置计算 ------------------------------ */
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int sat_gps_pos_clac(FILE * result_file,
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pnav_body nav_b, pobs_epoch obs_e, pobs_body obs_b,
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pobs_head obs_h, pstation station, ppos_t pos_t,
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pblh blh, penu enu, prah rah,
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int o_epochnum, int gps_satnum)
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/* ------------------------------- GPS卫星位置计算&输出 ------------------------------ */
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int sat_gps_pos_clac(FILE * result_file,
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pnav_body nav_b, pobs_epoch obs_e, pobs_body obs_b,
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pobs_head obs_h, pstation station, ppos_t pos_t,
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pblh blh, penu enu, prah rah,
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int o_epochnum, int gps_satnum)
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{ int progress = 0;
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int count = 0;
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pxyz2blh tem1 = NULL;
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@@ -149,9 +87,6 @@
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teml = (pdeg2dms)malloc(sizeof(pdeg2dms)* 512);
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for (int i = 0; i < o_epochnum; i++)//第i个历元
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{
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result_file = fopen(".\\Pos_out\\LLA_result_for_read.txt", "a+");
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fprintf(result_file, "\n>%04d %04d %02d %02d %02d %02d %07.04f",i + 1 ,obs_e[i].y ,obs_e[i].m ,obs_e[i].d ,obs_e[i].h ,obs_e[i].min ,obs_e[i].sec);
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fclose(result_file);
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@@ -187,12 +122,12 @@
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}
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/* ----------------------------- 地固坐标系转经纬大地高坐标系 ----------------------------- */
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tem1 = XYZ2BLH( tem1, pos_t[i].X[sPRN], pos_t[i].Y[sPRN], pos_t[i].Z[sPRN], a, e2);
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tem1 = XYZ2BLH( tem1, pos_t[i].X[sPRN], pos_t[i].Y[sPRN], pos_t[i].Z[sPRN]);
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blh->B = rad2deg(tem1->B);
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blh->L = rad2deg(tem1->L);
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blh->H = tem1->H;
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tem2 = XYZ2BLH( tem2, obs_h->apX, obs_h->apY, obs_h->apZ, a, e2);
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tem2 = XYZ2BLH( tem2, obs_h->apX, obs_h->apY, obs_h->apZ);
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station->B = tem2->B;
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station->L = tem2->L;
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station->H = tem2->H;
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@@ -254,10 +189,10 @@
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int progress_now = (int)(((i+1)*100/2880));
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if ((progress_now - progress)>=2)
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{
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printf("-");
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printf("=");
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count++;
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progress = progress_now;
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printf("-]%3d%%", progress);
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printf("=]%3d%%", progress);
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for(int countb = 0; countb < (5); countb++)
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{
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printf("\b");
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