?? globe.h
字號:
//typedef unsigned char Boolean ;
#define True 1
#define False 0
/********* type definitions *********/
typedef char i1; /* data type allowing for the use of 8 bits. */
typedef short i2; /* data type allowing for the use of 16 bits. */
typedef long i4; /* data type allowing for the use of 32 bits. */
typedef unsigned char u1; /* unsigned 8 bits */
typedef unsigned short u2; /* unsigned 16 bits */
typedef unsigned long u4; /* unsigned 32 bits */
typedef float r4;
typedef double r8;
/* emphric varition */
long TLW;
long HOW;
char URA;
int prn;
short wn; /* GPS week number */
long tow; /* sec of GPS week */
double tgd; /* grup delay (s)*/
long aodc; /* clock date issue */
long toc; /* clock data reference time(sec) */
double af2, /* clock correction(sec/sec2) */
af1, /* clock correction(sec/sec) */
af0; /* clock correction(sec) */
double alph0, /* ionospheric parameter(second) */
alph1, /* ionospheric parameter(sec/semi-circles) */
alph2, /* ionospheric parameter(s/semi-circles2) */
alph3, /* ionospheric parameter(s/semi-circles3) */
belta0, /* ionospheric parameter(s) */
belta1, /* ionospheric parameter(s/semi-circles) */
belta2, /* ionospheric parameter(s/semi-circles2) */
belta3; /* ionospheric parameter(s/semi-circles3) */
long aode,aode3; /* orbit date issue in subframes 2 and 3 */
double deltan; /* mean anomoly correction
semi-circles per sec*pi = rads */
double m0, /* mean anomoly at ref time
semi-circles*pi = rads */
e, /* eccentricity */
roota; /* sqr root a ( metres 1/2 ) */
long toe; /* ref time (sec) */
double cic, /* harmonic correction term(rads) */
crc, /* harmonic correction term(metres) */
cis, /* harmonic correction term(rads) */
crs, /* harmonic correction term(metres) */
cuc, /* harmonic correction term(rads) */
cus; /* harmonic correction term(rads) */
double omega0, /* longitude of asccending node
semi-circles*pi = rads */
omega, /* argument of perigee
semi-circles*pi */
i0; /* inclination angle at ref time
semi-circles*pi */
double omegadot, /* rate of right ascension
semi-circles/sec*pi */
idot; /* rate of inclination
semi-circles/sec*pi */
int accuracy, /* User range accuracy */
health, /* Satellite health */
fit; /* Curve fit interval */
char prnum; /* sv prn number */
char res; /* Reserved character */
unsigned checksum; /* check sum */
#define PI 3.1415926535898 /* GPS value of Pi */
#define WE 7.2921151467E-5 /* WGS84 earths rotation rate (rads/sec) */
#define SQRMU 1.99649818432174E7 /* Square root of MU. */
#define FCONST -4.442807633E-10 /* FCONST is used in relativistic clock
correction. Defined on pg. 73 of
ICD-GPS-200. */
#define TWOM5 0.03125000000000 /* 2^-5 */
#define TWOM11 (TWOM5 / 64.0)
#define TWOM12 (TWOM11 / 2.0)
#define TWOM19 (TWOM11 / 256.0)
#define TWOM20 (TWOM19 / 2.0)
#define TWOM21 (TWOM20 / 2.0)
#define TWOM23 (TWOM21 / 4.0)
#define TWOM24 (TWOM23 / 2.0)
#define TWOM27 (TWOM24 / 8.0)
#define TWOM29 (TWOM23 / 64.0)
#define TWOM30 (TWOM29 / 2.0)
#define TWOM31 (TWOM30 / 2.0)
#define TWOM33 (TWOM31 / 4.0)
#define TWOM38 (TWOM33 / 32.0)
#define TWOM43 (TWOM38 / 32.0)
#define TWOM50 (TWOM43 / 128.0)
#define TWOM55 (TWOM50 / 32.0)
#define TWOM3125 (0.25 * TWOM31)
#define TWOP11 2048.0 /* 2^11 */
#define TWOP12 (TWOP11 * 2.0)
#define TWOP14 (TWOP12 * 4.0)
#define TWOP16 (TWOP14 * 4.0)
#define TWOP12_INTEGER 4096 /* 2^12 */
#define TWOP16_INTEGER 65536 /* 2^16 */
#define PITWOM19 (PI * TWOM19)
#define PITWOM23 (PI * TWOM23)
#define PITWOM31 (PI * TWOM31)
#define PITWOM38 (PI * TWOM38)
#define PITWOM43 (PI * TWOM43)
?? 快捷鍵說明
復制代碼
Ctrl + C
搜索代碼
Ctrl + F
全屏模式
F11
切換主題
Ctrl + Shift + D
顯示快捷鍵
?
增大字號
Ctrl + =
減小字號
Ctrl + -