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+6
-1
@@ -1,5 +1,10 @@
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{
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"files.associations": {
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"unistd.h": "c"
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"unistd.h": "c",
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"select_epo.h": "c",
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"xyz2blh.h": "c",
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"deg2dms.h": "c",
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"blh2enu.h": "c",
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"terminal.h": "c"
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}
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}
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@@ -19343,7 +19343,7 @@ G12[sPRN] 8° 52′ 46″ 68° 05′ 27″ 20210521.21327
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G30[sPRN] -16° 03′ 27″ 178° 50′ 25″ 20290461.70428
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G05[sPRN] 17° 44′ 46″ 80° 37′ 42″ 20058204.33160
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G14[sPRN] -54° 30′ 08″ 168° 29′ 53″ 20202945.59449
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G17[sPRN] -23° 46′ 16″ 150° 41′ 08″ 20032545.37168
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G17[sPRN] -23° 46′ 16″ 150° 41′ 08″ 20032545.37167
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G07[sPRN] 3° 11′ 44″ -167° 24′ 02″ 20472840.48542
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G13[sPRN] -29° 17′ 16″ 115° 04′ 45″ 20188988.11695
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G19[sPRN] -9° 04′ 54″ 142° 15′ 47″ 20121519.14606
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File renamed without changes.
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@@ -19343,7 +19343,7 @@ G12[sPRN] 8.87968 68.09086 20210521.21327
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G30[sPRN] -16.05758 178.84031 20290461.70428
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G05[sPRN] 17.74627 80.62854 20058204.33160
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G14[sPRN] -54.50226 168.49819 20202945.59449
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G17[sPRN] -23.77119 150.68578 20032545.37168
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G17[sPRN] -23.77119 150.68578 20032545.37167
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G07[sPRN] 3.19562 -167.40058 20472840.48542
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G13[sPRN] -29.28788 115.07943 20188988.11695
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G19[sPRN] -9.08185 142.26320 20121519.14606
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+2
-1
@@ -1,5 +1,6 @@
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function [ENU] = Station_Site_Solving()
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% 打开坐标文件
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file=fopen('LLA_result_for_Matlab.txt');
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file=fopen('LLA_result.txt');
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sPRN = [];
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satX = [];
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satY = [];
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File renamed without changes.
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@@ -4,6 +4,8 @@
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#include<stdlib.h>
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#include<math.h>
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#include"public.h"
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#include"read.h"
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#include"2gpst.h"
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#include"select_epo.h"
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@@ -82,13 +84,13 @@ int sat_gps_pos_clac(FILE * result_file,
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station = (pstation)malloc(sizeof(pstation) * o_epochnum* 256);
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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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result_file = fopen(".\\Pos_out\\LLA_result.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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result_file = fopen(".\\Draw the Track[by PyGMT]\\LLA_result_for_PyGMT.txt", "a+");
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result_file = fopen(".\\PyGMT_out\\LLA_result.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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result_file = fopen(".\\Observation_Station_Site-Solving_by_Matlab\\LLA_result_for_Matlab.txt", "a+");
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result_file = fopen(".\\Result_out\\LLA_result.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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@@ -161,20 +163,20 @@ int sat_gps_pos_clac(FILE * result_file,
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blh->L_m = teml.M;
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blh->L_s = teml.S;
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result_file = fopen(".\\Pos_out\\LLA_result_for_read.txt", "a+");
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result_file = fopen(".\\Pos_out\\LLA_result.txt", "a+");
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fprintf(result_file, "\nG%02d[sPRN] %4d° %02d′ %02d″ %4d° %02d′ %02d″ %15.05f",sPRN, blh->B_d, blh->B_m, blh->B_s, blh->L_d, blh->L_m, blh->L_s, blh->H);
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fclose(result_file);
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result_file = fopen(".\\Draw the Track[by PyGMT]\\LLA_result_for_PyGMT.txt", "a+");
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result_file = fopen(".\\PyGMT_out\\LLA_result.txt", "a+");
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fprintf(result_file, "\nG%02d[sPRN] %10.05f %10.05f %15.05f",sPRN, blh->B, blh->L, blh->H);
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fclose(result_file);
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result_file = fopen(".\\Observation_Station_Site-Solving_by_Matlab\\LLA_result_for_Matlab.txt", "a+");
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result_file = fopen(".\\Result_out\\LLA_result.txt", "a+");
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fprintf(result_file, "\nG%02d[sPRN] %15.05f %15.05f %15.05f %15.05f %15.05f %15.05f %15.12f %16.13f"
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,sPRN, pos_t[i].X[sPRN], pos_t[i].Y[sPRN], pos_t[i].Z[sPRN], obs_b[i].obs_gps[j][C1], obs_b[i].obs_gps[j][10], rah->H, nav_b[best_epoch].TGD, pos_t[i].delta_clk[sPRN]);
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fclose(result_file);
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}
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}
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result_file = fopen(".\\Observation_Station_Site-Solving_by_Matlab\\LLA_result_for_Matlab.txt", "a+");
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result_file = fopen(".\\Result_out\\LLA_result.txt", "a+");
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fprintf(result_file, "\n");
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fclose(result_file);
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@@ -197,7 +199,7 @@ int sat_gps_pos_clac(FILE * result_file,
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/* -------------------------------------------------------------------------- */
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}
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result_file = fopen(".\\Observation_Station_Site-Solving_by_Matlab\\LLA_result_for_Matlab.txt", "a+");
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result_file = fopen(".\\Result_out\\LLA_result.txt", "a+");
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fprintf(result_file, "\nEND");
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fclose(result_file);
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free(blh);blh = NULL;
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File renamed without changes.
@@ -1,7 +1,7 @@
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#ifndef _DEGRRAD_H_
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#define _DEGRRAD_H_
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#include"read.h"
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#include"public.h"
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/* -------------------------------------------------------------------------- */
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/// @brief 角度转弧度
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@@ -0,0 +1,227 @@
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#ifndef _PUBLIC_H_
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#define _PUBLIC_H_
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/* ------------------------------ WGS-84 CONST ------------------------------ */
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#define a 6378137.0
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#define e2 (0.0033528106647475*(2 - 0.0033528106647475))
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#define C_V 299792458
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#define GM 398600500000000
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#define math_e 2.718281828459
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#define PI 3.141592653589793
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#define Earth_e 7.2921151467e-5
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#define C1 0
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/* ----------------------------- GPS OBSERV TYPE ---------------------------- */
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#define C1C 101
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#define C1S 102
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#define C1L 103
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#define C1X 104
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#define C1P 105
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#define C1W 106
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#define C1Y 107
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#define C1M 108
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#define C2C 201
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#define C2S 202
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#define C2L 203
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#define C2X 204
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#define C2P 205
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#define C2W 206
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#define C2Y 207
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#define C2M 208
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#define C5I 501
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#define C5Q 502
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#define C5X 503
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/* ------------------------------ FOR CALMOD.H ------------------------------ */
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#define MAXRINEX 1000
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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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//经纬高结构体
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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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//东北天结构体
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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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//高度方位角结构体
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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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/* ------------------------------- FOR READ.H ------------------------------- */
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//导航头文件结构体
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typedef struct nav_head
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{
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double ver;//rinex 版本号
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char type[20];//读取的数据类型
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double ION_GPSA[4];//8个电离层参数
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double ION_GPSB[4];
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double ION_BDSA[4];//8个电离层参数
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double ION_BDSB[4];
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double ION_QZSA[4];//8个电离层参数
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double ION_QZSB[4];
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double ION_IRNA[4];//8个电离层参数
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double ION_IRNB[4];
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double GPUT[4];
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double GLUT[4];
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double GAUT[4];
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double BDUT[4];
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double QZUT[4];
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double IRUT[4];
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double SBUT[4];
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int leap;
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}nav_head, *pnav_head;
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//导航数据结构体
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typedef struct nav_body
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{
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//数据块第一行内容:
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int sPRN;//卫星PRN号
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//历元:TOC中卫星钟的参考时刻
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int TOC_Y;//年
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int TOC_M;//月
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int TOC_D;//日
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int TOC_H;//时
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int TOC_Min;//分
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int TOC_Sec;//秒
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double sa0;//卫星钟差
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double sa1;//卫星钟偏
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double sa2;//卫星钟漂
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//数据块第二行内容:
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double IODE;//数据、星历发布时间(数据期龄)
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double Crs;//轨道半径的正弦调和改正项的振幅(单位:m)
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double deltan;//卫星平均运动速率与计算值之差(rad/s)
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double M0;//参考时间的平近点角(rad)
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//数据块第三行内容:
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double Cuc;//维度幅角的余弦调和改正项的振幅(rad)
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double e;//轨道偏心率
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double Cus;//轨道幅角的正弦调和改正项的振幅(rad)
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double sqrtA;//长半轴平方根
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//数据块第四行内容:
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double TOE;//星历的参考时刻(GPS周内秒)
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double Cic;//轨道倾角的余弦调和改正项的振幅(rad)
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double OMEGA;//参考时刻的升交点赤经
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double Cis;//维度倾角的正弦调和改正项的振幅(rad)
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//数据块第五行内容:
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double i0;//参考时间的轨道倾角(rad)
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double Crc;//轨道平径的余弦调和改正项的振幅(m)
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double omega;//近地点角距
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double deltaomega;//升交点赤经变化率(rad)
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//数据块第六行内容:
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double IDOT;//近地点角距(rad/s)
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double L2code;//L2上的码
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double GPSweek;//GPS周,于TOE一同表示
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double L2Pflag;//L2,p码数据标记
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//数据块第七行内容
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double sACC;//卫星精度
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double sHEA;//卫星健康状态
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double TGD;//sec
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double IODC;//钟的数据龄期
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//数据块第八行内容
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double TTN;//电文发送时间
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double fit;//拟合区间
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double spare1;//空
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double spare2;//空
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||||
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}nav_body, *pnav_body;
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//观测值头文件结构体
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typedef struct obs_head
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{
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double ver;//RINEX文件版本号
|
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char type[30];//文件类型
|
||||
double apX;//测站近似位置XYZ(WGS84)
|
||||
double apY;
|
||||
double apZ;
|
||||
double ANTH;//天线高
|
||||
double ANTdeltaE;//天线中心对于测站标志在东方向上的偏移量
|
||||
double ANTdeltaN;//天线中心对于测站标志在北方向上的偏移量
|
||||
int WAFL1;//缺省的L1载波的波长因子
|
||||
int WAFL2;//缺省的L2载波的波长因子
|
||||
int WAFflag;
|
||||
int obstypenum_gps;//GPS观测值类型数量
|
||||
int obstypenum_bds;
|
||||
char obstype_gps[36];//rinex3.04GPS观测值类型列表
|
||||
char obstype_bds[36];
|
||||
double interval;//观测值的历元间隔
|
||||
int f_y;//第一个观测记录的时刻
|
||||
int f_m;
|
||||
int f_d;
|
||||
int f_h;
|
||||
int f_min;
|
||||
double f_sec;
|
||||
char tsys[5];//时间系统
|
||||
}obs_head,*pobs_head;
|
||||
|
||||
|
||||
//观测值历元数据结构体
|
||||
typedef struct obs_epoch
|
||||
{
|
||||
//观测历元时刻
|
||||
int y;
|
||||
int m;
|
||||
int d;
|
||||
int h;
|
||||
int min;
|
||||
double sec;
|
||||
int p_flag;//历元标志
|
||||
int sat_num;//当前历元所观测到的卫星数量
|
||||
int gps_num;//当前历元所观测到的GPS卫星数量
|
||||
int bds_num;//当前历元所观测到的BDS卫星数量
|
||||
int sPRN[84];//当前历元所能观测到的卫星的PRN列表
|
||||
int sPRN_GPS[25];
|
||||
int sPRN_BDS[36];
|
||||
}obs_epoch,*pobs_epoch;
|
||||
|
||||
|
||||
//观测值数据结构体
|
||||
typedef struct obs_body
|
||||
{
|
||||
double obs_gps[100][24];//GPS观测值
|
||||
double obs_bds[100][24];//BDS观测值
|
||||
}obs_body,*pobs_body;
|
||||
/* -------------------------------------------------------------------------- */
|
||||
|
||||
#endif
|
||||
@@ -4,7 +4,7 @@
|
||||
#include<stdlib.h>
|
||||
#include<math.h>
|
||||
|
||||
#include"read.h"
|
||||
#include"public.h"
|
||||
|
||||
typedef struct
|
||||
{
|
||||
+1
-224
@@ -4,89 +4,7 @@
|
||||
#include<stdio.h>
|
||||
#include<string.h>
|
||||
|
||||
#define MAXRINEX 1000//一行最大字符数
|
||||
/* ------------------------------ WGS-84 CONST ------------------------------ */
|
||||
#define a 6378137.0
|
||||
#define e2 (0.0033528106647475*(2 - 0.0033528106647475))
|
||||
#define C_V 299792458
|
||||
#define GM 398600500000000
|
||||
#define math_e 2.718281828459
|
||||
#define PI 3.141592653589793
|
||||
#define Earth_e 7.2921151467e-5
|
||||
#define C1 0
|
||||
/* ----------------------------- GPS OBSERV TYPE ---------------------------- */
|
||||
#define C1C 101
|
||||
#define C1S 102
|
||||
#define C1L 103
|
||||
#define C1X 104
|
||||
#define C1P 105
|
||||
#define C1W 106
|
||||
#define C1Y 107
|
||||
#define C1M 108
|
||||
|
||||
#define C2C 201
|
||||
#define C2S 202
|
||||
#define C2L 203
|
||||
#define C2X 204
|
||||
#define C2P 205
|
||||
#define C2W 206
|
||||
#define C2Y 207
|
||||
#define C2M 208
|
||||
|
||||
#define C5I 501
|
||||
#define C5Q 502
|
||||
#define C5X 503
|
||||
/* ------------------------------ FOR CALMOD.H ------------------------------ */
|
||||
//卫星位置结构体
|
||||
typedef struct
|
||||
{
|
||||
double X[36];
|
||||
double Y[36];
|
||||
double Z[36];
|
||||
double deltat[36];//改正前的信号传播时间
|
||||
double delta_t[36];//改正后的信号传播时间
|
||||
double delta_clk[36];
|
||||
}pos_t, *ppos_t;
|
||||
|
||||
//测站位置结构体
|
||||
typedef struct
|
||||
{
|
||||
double X;
|
||||
double Y;
|
||||
double Z;
|
||||
double B;
|
||||
double L;
|
||||
double H;
|
||||
double delta_TR;
|
||||
}station, *pstation;
|
||||
//经纬高结构体
|
||||
typedef struct
|
||||
{
|
||||
double B;
|
||||
int B_d;
|
||||
int B_m;
|
||||
int B_s;
|
||||
double L;
|
||||
int L_d;
|
||||
int L_m;
|
||||
int L_s;
|
||||
double H;
|
||||
}blh, *pblh;
|
||||
//东北天结构体
|
||||
typedef struct enu
|
||||
{
|
||||
double E;
|
||||
double N;
|
||||
double U;
|
||||
}enu, *penu;
|
||||
//高度方位角结构体
|
||||
typedef struct rah
|
||||
{
|
||||
double R;
|
||||
double A;
|
||||
double H;
|
||||
}rah, *prah;
|
||||
|
||||
#include"public.h"
|
||||
/* ------------------------ 将字符串转换为浮点数,i起始位置,n输入多少个字符 ----------------------- */
|
||||
static double strtonum(const char* buff, int i, int n)
|
||||
{
|
||||
@@ -113,147 +31,6 @@ static double strtonum(const char* buff, int i, int n)
|
||||
return sscanf(str, "%lf", &value) == 1 ? value : 0.0;
|
||||
}
|
||||
|
||||
/* -------------------------------- 导航头文件结构体 -------------------------------- */
|
||||
typedef struct nav_head
|
||||
{
|
||||
double ver;//rinex 版本号
|
||||
char type[20];//读取的数据类型
|
||||
double ION_GPSA[4];//8个电离层参数
|
||||
double ION_GPSB[4];
|
||||
double ION_BDSA[4];//8个电离层参数
|
||||
double ION_BDSB[4];
|
||||
double ION_QZSA[4];//8个电离层参数
|
||||
double ION_QZSB[4];
|
||||
double ION_IRNA[4];//8个电离层参数
|
||||
double ION_IRNB[4];
|
||||
double GPUT[4];
|
||||
double GLUT[4];
|
||||
double GAUT[4];
|
||||
double BDUT[4];
|
||||
double QZUT[4];
|
||||
double IRUT[4];
|
||||
double SBUT[4];
|
||||
int leap;
|
||||
}nav_head, *pnav_head;
|
||||
|
||||
/* --------------------------------- 导航数据结构体 -------------------------------- */
|
||||
typedef struct nav_body
|
||||
{
|
||||
//数据块第一行内容:
|
||||
int sPRN;//卫星PRN号
|
||||
//历元:TOC中卫星钟的参考时刻
|
||||
int TOC_Y;//年
|
||||
int TOC_M;//月
|
||||
int TOC_D;//日
|
||||
int TOC_H;//时
|
||||
int TOC_Min;//分
|
||||
int TOC_Sec;//秒
|
||||
double sa0;//卫星钟差
|
||||
double sa1;//卫星钟偏
|
||||
double sa2;//卫星钟漂
|
||||
|
||||
//数据块第二行内容:
|
||||
double IODE;//数据、星历发布时间(数据期龄)
|
||||
double Crs;//轨道半径的正弦调和改正项的振幅(单位:m)
|
||||
double deltan;//卫星平均运动速率与计算值之差(rad/s)
|
||||
double M0;//参考时间的平近点角(rad)
|
||||
|
||||
//数据块第三行内容:
|
||||
double Cuc;//维度幅角的余弦调和改正项的振幅(rad)
|
||||
double e;//轨道偏心率
|
||||
double Cus;//轨道幅角的正弦调和改正项的振幅(rad)
|
||||
double sqrtA;//长半轴平方根
|
||||
|
||||
//数据块第四行内容:
|
||||
double TOE;//星历的参考时刻(GPS周内秒)
|
||||
double Cic;//轨道倾角的余弦调和改正项的振幅(rad)
|
||||
double OMEGA;//参考时刻的升交点赤经
|
||||
double Cis;//维度倾角的正弦调和改正项的振幅(rad)
|
||||
|
||||
//数据块第五行内容:
|
||||
double i0;//参考时间的轨道倾角(rad)
|
||||
double Crc;//轨道平径的余弦调和改正项的振幅(m)
|
||||
double omega;//近地点角距
|
||||
double deltaomega;//升交点赤经变化率(rad)
|
||||
|
||||
//数据块第六行内容:
|
||||
double IDOT;//近地点角距(rad/s)
|
||||
double L2code;//L2上的码
|
||||
double GPSweek;//GPS周,于TOE一同表示
|
||||
double L2Pflag;//L2,p码数据标记
|
||||
|
||||
//数据块第七行内容
|
||||
double sACC;//卫星精度
|
||||
double sHEA;//卫星健康状态
|
||||
double TGD;//sec
|
||||
double IODC;//钟的数据龄期
|
||||
|
||||
//数据块第八行内容
|
||||
double TTN;//电文发送时间
|
||||
double fit;//拟合区间
|
||||
double spare1;//空
|
||||
double spare2;//空
|
||||
|
||||
}nav_body, *pnav_body;
|
||||
|
||||
/* --------------------------------- 观测值头文件结构体 --------------------------------- */
|
||||
typedef struct obs_head
|
||||
{
|
||||
double ver;//RINEX文件版本号
|
||||
char type[30];//文件类型
|
||||
double apX;//测站近似位置XYZ(WGS84)
|
||||
double apY;
|
||||
double apZ;
|
||||
double ANTH;//天线高
|
||||
double ANTdeltaE;//天线中心对于测站标志在东方向上的偏移量
|
||||
double ANTdeltaN;//天线中心对于测站标志在北方向上的偏移量
|
||||
int WAFL1;//缺省的L1载波的波长因子
|
||||
int WAFL2;//缺省的L2载波的波长因子
|
||||
int WAFflag;
|
||||
int obstypenum_gps;//GPS观测值类型数量
|
||||
int obstypenum_bds;
|
||||
char obstype_gps[36];//rinex3.04GPS观测值类型列表
|
||||
char obstype_bds[36];
|
||||
double interval;//观测值的历元间隔
|
||||
int f_y;//第一个观测记录的时刻
|
||||
int f_m;
|
||||
int f_d;
|
||||
int f_h;
|
||||
int f_min;
|
||||
double f_sec;
|
||||
char tsys[5];//时间系统
|
||||
}obs_head,*pobs_head;
|
||||
|
||||
|
||||
/* ------------------------------- 观测值历元数据结构体 ------------------------------- */
|
||||
typedef struct obs_epoch
|
||||
{
|
||||
//观测历元时刻
|
||||
int y;
|
||||
int m;
|
||||
int d;
|
||||
int h;
|
||||
int min;
|
||||
double sec;
|
||||
int p_flag;//历元标志
|
||||
int sat_num;//当前历元所观测到的卫星数量
|
||||
int gps_num;//当前历元所观测到的GPS卫星数量
|
||||
int bds_num;//当前历元所观测到的BDS卫星数量
|
||||
int sPRN[84];//当前历元所能观测到的卫星的PRN列表
|
||||
int sPRN_GPS[25];
|
||||
int sPRN_BDS[36];
|
||||
}obs_epoch,*pobs_epoch;
|
||||
|
||||
|
||||
/* -------------------------------- 观测值数据结构体 -------------------------------- */
|
||||
typedef struct obs_body
|
||||
{
|
||||
double obs_gps[100][24];//GPS观测值
|
||||
double obs_bds[100][24];//BDS观测值
|
||||
}obs_body,*pobs_body;
|
||||
/* -------------------------------------------------------------------------- */
|
||||
|
||||
|
||||
/* -------------------------------------------------------------------------- */
|
||||
/* 读取O文件
|
||||
/* -------------------------------------------------------------------------- */
|
||||
@@ -3,7 +3,7 @@
|
||||
|
||||
#include<math.h>
|
||||
|
||||
#include"read.h"
|
||||
#include"public.h"
|
||||
|
||||
/* -------------------------------------------------------------------------- */
|
||||
/// @brief 寻找与观测历元最近的卫星广播历元
|
||||
File renamed without changes.
@@ -4,7 +4,7 @@
|
||||
#include<stdlib.h>
|
||||
#include<math.h>
|
||||
|
||||
#include"read.h"
|
||||
#include"public.h"
|
||||
|
||||
typedef struct
|
||||
{
|
||||
@@ -14,9 +14,9 @@
|
||||
#include<string.h>
|
||||
#include<unistd.h>
|
||||
|
||||
#include"read.h"
|
||||
#include"cal_mod.h"
|
||||
#include"terminal.h"
|
||||
#include"headers/read.h"
|
||||
#include"headers/cal_mod.h"
|
||||
#include"headers/terminal.h"
|
||||
|
||||
int main(void)
|
||||
{
|
||||
|
||||
Reference in new issue
Block a user