home
***
CD-ROM
|
disk
|
FTP
|
other
***
search
/
HAM Radio 1
/
HamRadio.cdr
/
satel
/
seesats
/
seesats.c
next >
Wrap
C/C++ Source or Header
|
1988-11-10
|
31KB
|
1,253 lines
/******************************************************************************
*
* SEESATS.C - Allows user to "see" where the satellites
* are currently located.
*
* Translated from W0SL's ORBITS2.BAS (BASIC) by:
*
* (c) Copyright
* November 1985
* Rich Bono - NM1D
* 7 Redfield Circle
* Derry, New Hampshire 03038
* (603) 432-9002
*
* **** Wild Mean Bits ****
*
* This program in its entirety, or in its parts, is NOT in the public
* domain. My Name/call/copyright must remain in both the source, and
* any executable produced from this source or any derivitive of it.
* Of course, if you make additions, you may add your name to the end
* of the copyright messages.
* This source is being made available to others to foster the goodwill
* and development of Amateur Radio satelellite operators. If you make
* any changes to this code, either for to port this to another machine
* or architechture, you must send me the source for archival reasons,
* and so that I can incorporate improvements into the reference copy.
*
*
*
* Note: This program is in such poor shape because it is a
* (almost) a direct translation from a BASIC source! I did all
* I could to disolve the spagetti sauce. With more time, and
* revisions, the code will improve....
*
* Revisions:
* Ver 1.0 25-Oct-88 localtime() was returning month as
* base 0, needed base 1
*
* Ver 0.9 19-Oct-88 Changed dos ints to calls to time(),
* and localtime()
* also changed for UNIX portability
*
* Ver 0.8 16-Feb-88 Fixed sat loop, so not to repeat
* selected bird
*
* Ver 0.7 13-Feb-88 Changes to read data file routine
*
* Ver 0.6 28-Dec-87 Fixed bug caused by MSC V4.0 float
* logic
*
* Ver 0.5 30-Sep-87 Added paged output mode logic,
* changed abs() to fabs()
*
* 22-May-87 Added argument driven loops
* 20-May-87 Added satelite data display
* 15-May-87 Changed menu operation to toggle.
*
* 06-May-87 Added Version display & concatenated
* data files to use SEESATS.DAT
*
* 13-Apr-87 Added prediction algorithms
* 28-Sep-86 Worked on variable names
*
* Hope to add/change:
*
* Doppler correction, outputs to drive az-el antenna control.
* Make bird data into structure.
* Get RID of all these *GLOBALS*!!
*
* Notes:
*
* This code was kept as generic as possible, that is, NO terminal
* control features were used to allow this to be fairly portable.
*
* Currently compiles with Microsoft-C, see GetAKeyNoEcho() for
* possible non-portable code.
*
* Set the FORMSDOS or FORUNIX flag as appropriate
*
* This has been tested under MS-DOS and OS/2
*/
#define VERSION "1.0" /* Version as displayed by program */
#include <stdio.h>
#include <math.h>
#include <time.h>
#include <ctype.h>
#define FORMSDOS 1 /* 1 = for MSDOS or OS/2 */
#define FORUNIX 0 /* 1 = for UNIX */
/* #define fopen fpopen /* open files with aid of MS-DOS PATH */
#define DATAFILE "seesats.dat" /* file that contains station & */
/* bird information */
#define bool int
#define ESC 27 /* Escape key */
#define TRUE (1)
#define FALSE (0)
#define abs(a) (((a) < 0) ? -(a) : (a))
#define MAXTRACKED 20 /* maximum number of satellites */
/************ GLOBALs ****************/
double pi = 3.1415926535; /* P1 value of PI */
double pi_2; /* P2 PI squared */
double pi_180; /* P0 PI/180 */
double one3rd = 1.0/3.0; /* one third */
double e_radius = 6378.16; /* R0 Earth's radius */
double e_flat = 298.16; /* F 1/Earth flattening */
/* coeficient */
double e_gm =75369793000000.0;/* G0 GM of Earth in */
/* (Orbits/day)^2/km^3 */
double stn_latitude; /* L9 station latitude */
double stn_longitude; /* W9 station longitude */
double stn_height; /* H9 station altitude */
char stn_call[8+1]; /* C$ station call sign */
int stn_utc; /* Number of hours to change to */
/* UTC from local time */
int s_year1[20+1]; /* Y1 siderial year info */
int s_year2; /* X2 */
double s_year3[20+1]; /* G3 */
double s_ratio = 1.0027379093; /* G1 Sidereal/Solar time */
/* rate ratio */
char sat_name[MAXTRACKED+1][10]; /* I$ sat name */
double beacon_freq[MAXTRACKED+1]; /* F1 */
double epoch_orbit[MAXTRACKED+1]; /* K0 */
int epoch_yr[MAXTRACKED+1]; /* Y3 */
double epoch_day[MAXTRACKED+1]; /* T0 */
double raan[MAXTRACKED+1]; /* O0 */
double inclination[MAXTRACKED+1]; /* I0 */
double eccentricity[MAXTRACKED+1]; /* E0 */
double arg_of_perigee[MAXTRACKED+1]; /* W0 */
double mean_anomoly[MAXTRACKED+1]; /* M0 */
double mean_motion[MAXTRACKED+1]; /* N0 */
double decay_rate[MAXTRACKED+1]; /* N1 */
double eccent,
realtime,
sat_orbit,
orbit_pi2,
sat_height,
this_orbit,
cos_eccent,
sin_eccent,
sat_latitude,
sat_range,
sat_longitude,
cos_s_lon,
s_lat_pi180,
sin_s_lon,
sat_azimuth,
sin_s_lat,
sat_elevation,
s_h_radis,
cos_s_lat,
sat_phase,
stn_x,
stn_y,
stn_z;
int max_sats;
int sider_cnt;
struct {
int hour;
int minute;
int second;
int tenth;
} static_time;
struct {
int year;
int month;
int day;
} static_date;
int dos_time = TRUE; /* when true read dos clock, else increment */
/* clock by min_inc */
int min_inc = 10; /* number of minutes to increment clock by */
int in_view = FALSE;/* when TRUE, only print data is sat is in view */
int aos_los = FALSE;/* when TRUE, only print data at (near) AOS/LOS */
int sel_bird = 0; /* when not 0, only use selected satelite */
int page_mode = TRUE; /* when TRUE, give user a page at a time */
/*****************************************************************************
*
* GetAKeyNoEcho() - read one key without echo
*
* if no input available return (0)
*
* else return key
*
* Note: this will not allow the NUL (CTRL-@) character to be input
*
*/
int GetAKeyNoEcho()
{
#if FORMSDOS
if(kbhit())
{
return(getch()); /* read key without echo */
}
else
{
return(0); /* no key to read */
}
#endif /* FORMSDOS */
#if FORUNIX
#include <termio.h>
struct termio tty, savetty;
int stat;
char keyin;
if(isatty(fileno(stdin)))
{
ioctl(fileno(stdin), TCGETA, &tty); /* read current settings */
savetty = tty; /* save current settings */
tty.c_lflag &= ~ (ICANON|ECHO); /* allow read of char without echo */
tty.c_cc[VMIN] = 0; /* allow read without blocking */
tty.c_cc[VTIME] = 0; /* no input timer */
ioctl(fileno(stdin), TCSETA, &tty); /* set new parameters */
}
stat = read(fileno(stdin), &keyin, 1); /* read one character */
if(isatty(fileno(stdin)))
{
ioctl(fileno(stdin), TCSETA, &savetty); /* restore previous settings */
}
return(stat ? ((int) keyin) : 0); /* return key read if any, else return 0 */
#endif /* FORUNIX */
} /* end of GetAKeyNoEcho() */
/****************************************************************************/
main(argc, argv)
int argc;
char *argv[];
{
FILE *fp, *fopen();
int hour(), minute(), second(), day(), month(), year();
int status;
int loops; /* number of loops to perform */
int forever; /* flag, is loops decremented? */
char *date();
char buffer[132];
register sat_number;
printf("\nSeesats version %s - (c) Copyright 1985 - By Rich Bono, NM1D.\n\n", VERSION);
/*********************************/
/* read earth station parameters */
/*********************************/
fp = fopen(DATAFILE,"r");
if(!fp)
{
fprintf(stderr, "\nFile %s missing!\n\n", DATAFILE);
exit(1);
}
do /* eat any comment lines, output note lines */
{
fgets(buffer, sizeof(buffer), fp);
if(buffer[0] == '|') /* output lines that begin with | */
{ /* to stdout */
printf("%s", &buffer[1]);
}
} while (buffer[0] == ';' || buffer[0] == '|');
if( 5 != sscanf(buffer, "%lf %lf %lf %s %d",
&stn_latitude, &stn_longitude, &stn_height,
stn_call, &stn_utc)
)
{
fprintf(stderr,"\nError reading file %s for earth station information!\n\n", DATAFILE);
fprintf(stderr,"Should be latitude longitude height station ID and UTC correction\n");
fprintf(stderr,"%lf %lf %lf %s %d\n",
&stn_latitude, &stn_longitude, &stn_height,stn_call, stn_utc);
fclose(fp);
exit(1);
}
fprintf(stderr,"Earth location data entered for '%s'.\n\n", stn_call);
/************************/
/* initialize constants */
/************************/
pi_2 = 2.0 * pi;
pi_180 = pi / 180.0;
e_flat = 1.0 / e_flat;
s_lat_pi180 = stn_latitude * pi_180;
sin_s_lat = sin(s_lat_pi180);
cos_s_lat = cos(s_lat_pi180);
sin_s_lon = sin( -stn_longitude * pi_180);
cos_s_lon = cos(stn_longitude * pi_180);
s_h_radis = e_radius * ( 1.0 - (e_flat / 2.0) + (e_flat / 2.0) * cos(2.0 * s_lat_pi180)) + stn_height / 1000.0;
s_lat_pi180 = atan( ((1.0 - e_flat)*(1.0 - e_flat)) * sin_s_lat / cos_s_lat);
stn_z = s_h_radis * sin(s_lat_pi180);
stn_x = s_h_radis * cos(s_lat_pi180) * cos_s_lon;
stn_y = s_h_radis * cos(s_lat_pi180) * sin_s_lon;
dos_time = TRUE;
settime(); /* initialize time and date structures */
/**********************************/
/* Initialize Sidereal time table */
/**********************************/
for(sider_cnt=1; sider_cnt<20; sider_cnt++)
{
s_year1[sider_cnt] = sider_cnt + 1980;
s_year2 = floor( (s_year1[sider_cnt] - 1.0) / 100.0);
s_year3[sider_cnt] = 2.0 - s_year2 + floor(s_year2 / 4.0) +
floor(365.25 * (s_year1[sider_cnt]-1.0)) +
floor(30.6001 * 14);
s_year3[sider_cnt] = (s_year3[sider_cnt] - 730550.5) / 36525;
s_year3[sider_cnt] = (s_year3[sider_cnt] * (s_year3[sider_cnt] * (s_year3[sider_cnt] *
(-7.1759593E-11) + .00000107759259) +
100.002139)) + .279057273;
s_year3[sider_cnt] = s_year3[sider_cnt] - floor(s_year3[sider_cnt]);
s_year1[sider_cnt] = s_year1[sider_cnt] - 1900;
}
/*******************************/
/* initialize satellite matrix */
/*******************************/
for(max_sats=1; max_sats<=MAXTRACKED; )
{
fgets(buffer, sizeof(buffer), fp);
/* skip lines that begin with a ';' or '|' */
/* output lines that begin with a '|; to stdout */
if(buffer[0] == ';' || buffer[0] == '|')
{
if(buffer[0] == '|')
{
printf("%s",&buffer[1]);
}
continue;
}
status = sscanf(buffer,"%s %d %lf %lf %lf %lf %lf %lf %lf %lf %lf %lf",
sat_name[max_sats],
&epoch_yr[max_sats],
&epoch_day[max_sats],
&inclination[max_sats],
&raan[max_sats],
&eccentricity[max_sats],
&arg_of_perigee[max_sats],
&mean_anomoly[max_sats],
&mean_motion[max_sats],
&decay_rate[max_sats],
&epoch_orbit[max_sats],
&beacon_freq[max_sats]
);
if(feof(fp) || (status != 12))
{
break;
}
fprintf(stderr,"Data for %2d satellite%s read.\r",max_sats,(max_sats==1?" ":"s"));
/*
* printf("%s %d %lf %lf %lf %lf %lf %lf %lf %lf %lf %lf\n",
* sat_name[max_sats],
* epoch_yr[max_sats],
* epoch_day[max_sats],
* inclination[max_sats],
* raan[max_sats],
* eccentricity[max_sats],
* arg_of_perigee[max_sats],
* mean_anomoly[max_sats],
* mean_motion[max_sats],
* decay_rate[max_sats],
* epoch_orbit[max_sats],
* beacon_freq[max_sats]
* );
*/
if(!((epoch_yr[max_sats] == year()) || (epoch_yr[max_sats] == year()-1)))
{
fprintf(stderr, "\nThe elements for satellite #%d (%s) is not from the\n", max_sats, sat_name[max_sats]);
fprintf(stderr, " current or preceding year. The current date is %s. Set the\n",date());
fprintf(stderr, " system date or update the satellite orbital elements.\n");
exit(1); /* back to menu if any */
}
max_sats++;
} /* end of for(max_sats=1; max_sats<=MAXTRACKED;) */
if(!page_mode)
{
fprintf(stderr, "\n\n Press [ENTER] for menu . . .\n");
}
else
{
printf("\n");
}
/********************************/
/* Orbit calculation loop */
/********************************/
switch(argc)
{
default:
case 1: /* no command line, set up to run forever */
dos_time = TRUE;
loops = 1;
forever = TRUE;
break;
case 2:
loops = atoi(argv[1]); /* get number of loops */
if(loops > 0) /* if legal number */
{
forever = FALSE; /* won't be running long*/
}
else
{
forever = TRUE; /* will never end */
}
dos_time = TRUE; /* be in realtime mode */
break;
} /* end of switch(argc) */
while(loops)
{
if(!dos_time) /* if not in realtime */
{
settime(); /* calculate date & time here */
}
if(sel_bird) /* if one bird */
{
if(GetAKeyNoEcho())
{
do_command(); /* give menu commands */
}
calc_orbit(sel_bird); /* calculate orbital data */
show_data(sel_bird); /* show current data */
}
else /* do all birds */
{
for(sat_number=1;sat_number < max_sats; sat_number++)
{
if(GetAKeyNoEcho())
{
do_command(); /* give menu commands */
}
calc_orbit(sat_number); /* calculate orbital data */
show_data(sat_number); /* show current data */
} /* end for(sat_number=1;sat_number < max_sats; sat_number++) */
}
if(!forever) /* if not running forever */
{
loops--; /* count this loop */
}
} /* end while(loops) */
} /* end of main() */
/*****************************************************************************
*
* calc_orbit() - calculate orbital data
*
*/
calc_orbit(sat_number)
register sat_number;
{
register loop_cnt;
bool calc;
int hour(), minute(), second(), day(), month(), year();
char *date();
double c[3+1][2+1];
double xx,
yy,
zz,
a0,
c0,
m0,
n0,
o0,
q0,
s0,
w0,
x_0,
y_0,
c1,
e1,
m1,
s1,
x1,
y_1,
z1,
c2,
e2,
g2,
k2,
s2,
r3,
b5,
c5,
m5,
s5,
x5,
y5,
z5,
c7,
g7,
s7,
x8,
y8,
z8;
double temp;
n0 = mean_motion[sat_number] + 2.0 * (realtime - epoch_day[sat_number]) * decay_rate[sat_number];
a0 = pow((e_gm / (n0 * n0)), one3rd);
e2 = 1.0 - eccentricity[sat_number] * eccentricity[sat_number];
e1 = sqrt(e2);
q0 = mean_anomoly[sat_number] / 360.0 + epoch_orbit[sat_number];
k2 = 9.95 * pow((e_radius / a0), 3.5) / (e2 * e2);
s1 = sin(inclination[sat_number] * pi_180);
c1 = cos(inclination[sat_number] * pi_180);
calc_time(sat_number); /* update realtime for this bird */
o0 = raan[sat_number] - (realtime - epoch_day[sat_number]) * k2 * c1;
s0 = sin(o0 * pi_180);
c0 = cos(o0 * pi_180);
w0 = arg_of_perigee[sat_number] + ( realtime - epoch_day[sat_number]) * k2 *
(2.5 * (c1 * c1) - .5);
s2 = sin(w0 * pi_180);
c2 = cos(w0 * pi_180);
c[1][1] = /*+*/(c2 * c0) - (s2 * s0 * c1);
c[1][2] = -(s2 * c0) - (c2 * s0 * c1);
c[2][1] = /*+*/(c2 * s0) + (s2 * c0 * c1);
c[2][2] = -(s2 * s0) + (c2 * c0 * c1);
c[3][1] = /*+*/(s2 * s1);
c[3][2] = /*+*/(c2 * s1);
this_orbit = (mean_motion[sat_number] + decay_rate[sat_number] * (realtime - epoch_day[sat_number])) *
(realtime - epoch_day[sat_number]) + q0;
sat_orbit = floor(this_orbit);
sat_phase = floor((this_orbit-sat_orbit) * 256.0);
orbit_pi2 = (this_orbit - sat_orbit) * pi_2;
eccent = orbit_pi2 + eccentricity[sat_number] * sin(orbit_pi2) + .5 *
(eccentricity[sat_number] * eccentricity[sat_number]) * sin(2.0 * orbit_pi2);
calc = TRUE;
while(calc) /* calculating */
{
sin_eccent = sin(eccent);
cos_eccent = cos(eccent);
r3 = 1.0 - eccentricity[sat_number] * cos_eccent;
m1 = eccent - eccentricity[sat_number] * sin_eccent;
m5 = m1 - orbit_pi2;
if( fabs(m5) < .000001)
{
calc = FALSE;
}
else
{
eccent = eccent - m5 / r3;
}
} /* end while(TRUE) calc */
x_0 = a0 * (cos_eccent - eccentricity[sat_number]);
y_0 = a0 * e1 * sin_eccent;
sat_height = a0 * r3;
x1 = x_0 * c[1][1] + y_0 * c[1][2];
y_1 = x_0 * c[2][1] + y_0 * c[2][2];
z1 = x_0 * c[3][1] + y_0 * c[3][2];
for(loop_cnt = 1; loop_cnt != sider_cnt; loop_cnt++)
{
if(epoch_yr[sat_number] == s_year1[loop_cnt])
{
g2 = s_year3[loop_cnt];
}
}
g7 = realtime * s_ratio + g2;
temp = g7; /* this is to force FWAIT by MSC V4.0! */
g7 = (g7 - floor(g7)) * pi_2;
s7 = -sin(g7);
c7 = cos(g7);
xx = /*+*/(x1 * c7) - (y_1 * s7);
yy = /*+*/(x1 * s7) + (y_1 * c7);
zz = z1;
x5 = (xx - stn_x);
y5 = (yy - stn_y);
z5 = (zz - stn_z);
sat_range = sqrt(x5 * x5 + y5 * y5 + z5 * z5);
z8 = /*+*/(x5 * cos_s_lon * cos_s_lat) + (y5 * sin_s_lon * cos_s_lat) + (z5 * sin_s_lat);
x8 = -(x5 * cos_s_lon * sin_s_lat) - (y5 * sin_s_lon * sin_s_lat) + (z5 * cos_s_lat);
y8 = /*+*/(y5 * cos_s_lon) - (x5 * sin_s_lon);
s5 = z8/sat_range;
c5 = sqrt(1.0 - s5 * s5);
sat_elevation = atan(s5 / c5) / pi_180;
if(x8 < 0.0)
{
sat_azimuth = pi + atan(y8 / x8);
}
else
{
if(x8 > 0.0 && y8 >= 0.0)
{
sat_azimuth = atan(y8/x8);
}
else
{
if(x8 > 0.0)
{
sat_azimuth = pi_2 + atan(y8/x8);
}
else
{
if(y8 < 0.0)
{
sat_azimuth = 3.0 * pi / 2.0;
}
else
{
sat_azimuth = pi / 2.0;
}
}
}
}
sat_azimuth = sat_azimuth / pi_180;
if(xx < 0.0)
{
sat_longitude = pi + atan(yy/xx);
}
else
{
if(xx > 0.0 && yy >= 0.0)
{
sat_longitude = atan(yy/xx);
}
else
{
if(xx > 0.0)
{
sat_longitude = pi_2 + atan(yy / xx);
}
else
{
if(yy < 0.0)
{
sat_longitude = 3.0 * pi/2.0;
}
else
{
sat_longitude = pi / 2.0;
}
}
}
}
sat_longitude = 360.0 - sat_longitude / pi_180;
b5 = zz / sat_height;
sat_latitude = atan(b5 / (sqrt(1 - (b5 * b5)))) / pi_180;
} /* end of calc_obit() */
/****************************************************************************
*
* show_data() - show current calculated data
*
* output a header line for each new day, and for each 'page'
*/
show_data(sat_number)
register sat_number;
{
char *stime(), *date();
char buffer[80];
static line = 0;
static oldday = 0;
if(
(in_view && (sat_elevation < 0.0))
)
{
return;
}
if((line-- <= 0) || (oldday != day()))
{
oldday = day();
line = MAXTRACKED-1;
if(page_mode)
{
fprintf(stderr, "\n-- [ENTER] to continue, M for menu -- ");
fgets(buffer, sizeof(buffer), stdin);
if(tolower(buffer[0])=='m') /* if user wants back to menu */
{
do_command(); /* handle command */
return;
}
}
printf("\nFor %8s, at %7.3f Latitude, %7.3f Longitude, %7.2f M Altitude",
stn_call,
stn_latitude,
stn_longitude,
stn_height
);
printf("\nSatellite Az El RngKm AltKm Lat Long Orbit Ph Beacon %s\n",date());
}
printf("%-10s %3.0f %3.0f %5.0f %5.0f %5.1f %5.1f %6.0f %4.0f %7.3f %s\n",
sat_name[sat_number], /* Name */
sat_azimuth, /* Azimuth */
sat_elevation, /* Elevation */
sat_range, /* Range_Km */
(sat_height - e_radius), /* Height_Km */
sat_latitude, /* Latitude */
sat_longitude, /* Longitude */
sat_orbit, /* Orbit */
sat_phase, /* Phase */
beacon_freq[sat_number], /* Freq (someday doppler corrected)*/
stime()
);
} /* end of show_data() */
/*******************************************************************************
*
* show_elements(sat) - display current element data for sat.
*
*
*/
show_elements(sat)
int sat;
{
printf("\n");
printf("Name : %9s\n", sat_name[sat]);
printf("Epoch year : %9d\n",
(epoch_yr[sat]<1900 ? epoch_yr[sat] + 1900 : epoch_yr[sat]));
printf("Epoch day : %20.10lf\n", epoch_day[sat]);
printf("Epoch orbit : %20.10lf\n", epoch_orbit[sat]);
printf("Inclination : %20.10lf\n", inclination[sat]);
printf("RAAN : %20.10lf\n", raan[sat]);
printf("Eccentricity : %20.10lf\n", eccentricity[sat]);
printf("Argument of perigee : %20.10lf\n", arg_of_perigee[sat]);
printf("Mean anomoly : %20.10lf\n", mean_anomoly[sat]);
printf("Mean motion : %20.10lf\n", mean_motion[sat]);
printf("Decay rate : %20.10lf\n", decay_rate[sat]);
printf("Beacon frequency : %20.10lf\n", beacon_freq[sat]);
printf("\n");
} /* end of show_elements() */
/*******************************************************************************
*
* do_command() - Handle any keyboard entries
* Present menu.
*
*/
do_command()
{
int index;
int cmd_loop;
char buffer[85];
cmd_loop = TRUE; /* keep looping until user is done */
/* with menu */
do
{
fprintf(stderr, "\n\n\t\t\t Current selections:\n");
/* the 3 fields for the following are : 10 chars for description, 16 chars data... */
fprintf(stderr,"\nMode is...%-16s Print...%-16s Select..%-16s\n",
(dos_time ? "realtime" : "prediction"),
(in_view ? "when in view" : "all calculations"),
(sel_bird ? sat_name[sel_bird] : "all satelites")
);
fprintf(stderr, "Output is.%-16s\n",
(page_mode ? "paged" : "continuous")
);
fprintf(stderr, "\n\n\t\t\tSeesats menu -\n\n");
fprintf(stderr, "\t\t1 - Mode to %s\n", (dos_time ? "prediction":"realtime"));
fprintf(stderr, "\t\t2 - Print %s\n",(in_view ? "all calculations" : "when in view"));
fprintf(stderr, "\t\t3 - Select %s\n",(sel_bird ? "all satelites" : "satelite of interest"));
fprintf(stderr, "\t\t4 - Print current element data for satelites\n");
fprintf(stderr, "\t\t5 - Change output mode to %s\n", (page_mode ? "continuous" : "paged"));
fprintf(stderr, "\n\t\t0 - Quit.\n\n");
fprintf(stderr, "Enter number for desired function ([ENTER] to continue) : ");
fgets(buffer, sizeof(buffer), stdin);
switch(buffer[0])
{
case '1': /* select either realtime or predictions */
dos_time = !dos_time; /* toggle mode */
if(dos_time)
{
fprintf(stderr,"\n\nRunning in realtime . . .\n");
settime();
}
else
{
fprintf(stderr, "\n\n\nEnter start day, month & year [ENTER = %02d/%02d/%02d ] (dd/mm/yy) : ",
static_date.day, static_date.month, static_date.year-1900);
fgets(buffer, sizeof(buffer), stdin);
if(strlen(buffer))
{
sscanf(buffer, "%d/%d/%4d",&static_date.day, &static_date.month, &static_date.year);
}
if(static_date.year < 1900)
{
static_date.year += 1900;
}
fprintf(stderr, "\nEnter start hour & minute [ENTER = %02d:%02d ] (hh:mm) : ",
static_time.hour, static_time.minute);
static_time.second = 0;
static_time.tenth = 0;
fgets(buffer, sizeof(buffer), stdin);
if(strlen(buffer))
{
sscanf(buffer, "%d:%d", &static_time.hour, &static_time.minute);
}
fprintf(stderr, "\nEnter number of minutes to increment [ENTER = %3d ] : ", min_inc);
fgets(buffer, sizeof(buffer), stdin);
if(strlen(buffer))
{
sscanf(buffer, "%d",&min_inc);
}
} /* end of if(dos_time) */
break;
case '2': /* select only in view or all calculations */
in_view = !in_view;
if(in_view)
{
fprintf(stderr,"\n\nWill show data for satelites only when in view . . .\n");
}
else
{
fprintf(stderr,"\n\nWill show all calculated data.\n");
}
break;
case '3': /* select bird of interest */
if(sel_bird)
{
sel_bird = 0;
fprintf(stderr,"\n\nShow data for all satelites.\n");
}
else
{
fprintf(stderr, "\n\nSelect from the following list :\n\n");
do
{
fprintf(stderr, "\t\t 0 = All the following\n");
for(index=1; index < max_sats; index++)
{
fprintf(stderr, "\t\t%2d = %s\n",index, sat_name[index]);
}
fprintf(stderr, "\n\n\t\tSelect satelite by number [ENTER = %d] : ", sel_bird);
fgets(buffer, sizeof(buffer), stdin);
if(strlen(buffer))
{
sscanf(buffer, "%d",&sel_bird);
}
} while ((sel_bird >= max_sats) || (sel_bird < 0));
} /* end of if(sel_bird) */
break;
case '4': /* display element data for bird(s) */
fprintf(stderr, "\n\nSelect from the following list to display current element data:\n\n");
do
{
fprintf(stderr, "\t\t 0 = All the following\n");
for(index=1; index < max_sats; index++)
{
fprintf(stderr, "\t\t%2d = %s\n",index, sat_name[index]);
}
fprintf(stderr, "\n\n\t\tSelect satelite by number [ENTER = %d] : ", 0);
fgets(buffer, sizeof(buffer), stdin);
if(strlen(buffer))
{
index=0;
sscanf(buffer, "%d",&index);
}
else
{
index = 0;
}
} while ((index >= max_sats) || (index < 0));
if(index)
{
show_elements(index); /* show current data for selected bird */
} else
{
for(index=1; index<max_sats; index++)
{
show_elements(index); /* show current data for all birds */
}
}
fprintf(stderr, "\n\n\tHit [ENTER] to continue : ");
fgets(buffer, sizeof(buffer), stdin);
break;
case '5': /* select paged or continuous output mode */
page_mode = !page_mode;
if(page_mode)
{
fprintf(stderr,"\n\nOutput mode changed to continuous output\n");
}
else
{
fprintf(stderr,"\n\nOutput mode changed to paged output\n");
}
break;
case '0':
fprintf(stderr, "\n\nSeeSats: done.\n\n");
exit(0);
break;
default:
cmd_loop = FALSE;
break;
} /* end of switch(buffer[0]) */
} while (cmd_loop); /* until done with command loop */
if(in_view) /* if in_view mode, machine may appear dead, tell user */
{
fprintf(stderr, "\nNOTE: There will be NOTHING displayed when none are in view!\n");
}
fprintf(stderr, "\n\n");
} /* end of do_command() */
/*********************************************
*
* Real time functions
*
*/
settime() /* set the static_time structure to the current time */
{
long l_systemtime;
struct tm *st_systemtime;
extern struct static_time;
register int carry;
static int days_in_mnth[13] =
{
0,
31,
28,
31,
30,
30,
30,
31,
31,
30,
31,
30,
31
};
if(dos_time) /* read DOS clock */
{
time(&l_systemtime); /* read the current system time */
st_systemtime = localtime(&l_systemtime); /* convert to parts */
static_time.hour = st_systemtime->tm_hour;
/* add UTC offset */
static_time.hour += stn_utc;
static_time.minute = st_systemtime->tm_min;
static_time.second = st_systemtime->tm_sec;
static_time.tenth = 0;
/* year should include century, ie: 1988 not 88 */
static_date.year = st_systemtime->tm_year + 1900;
/* month should be 1 through 12, 1 = January */
static_date.month = st_systemtime->tm_mon + 1;
/* day is day of the month, 1 - 31 */
static_date.day = st_systemtime->tm_mday;
}
else /* increment time/date by min_inc */
{
if((static_date.year % 4) == 0)
{
days_in_mnth[2] = 29;
}
else
{
days_in_mnth[2] = 28;
}
static_time.tenth = 0;
static_time.second = 0;
static_time.minute += min_inc;
}
/* adjust rollover of time if needed */
carry = static_time.minute/60;
static_time.minute %= 60;
static_time.hour += carry;
carry = static_time.hour/24;
static_time.hour %= 24;
static_date.day += carry;
carry = static_date.day/(days_in_mnth[static_date.month]+1);
static_date.day %= (days_in_mnth[static_date.month]+1);
if(static_date.day == 0)
{
static_date.day = 1;
}
static_date.month += carry;
carry = static_date.month/13;
static_date.month %= 13;
if(static_date.month == 0)
{
static_date.month = 1;
}
static_date.year += carry;
} /* end of settime() */
int second() /* return seconds part of clock */
{
extern struct static_time;
return(static_time.second);
}
int minute() /* return minutes part of clock */
{
extern struct static_time;
return(static_time.minute);
}
int hour() /* return hours part of clock */
{
extern struct static_time;
return(static_time.hour);
}
int day() /* return day of month */
{
extern struct static_date;
return(static_date.day);
}
int month() /* return month of year */
{
extern struct static_date;
return(static_date.month);
}
int year() /* return year */
{
extern struct static_date;
return(static_date.year - 1900);
}
char *date() /*return date in string format (ie: 23-Feb-86) */
{
static char date[20];
static char *mnth[13] = { "***",
"Jan",
"Feb",
"Mar",
"Apr",
"May",
"Jun",
"Jul",
"Aug",
"Sep",
"Oct",
"Nov",
"Dec"
};
sprintf(date,"%02d-%s-%02d",day(),mnth[month()],year());
return(date);}
char *stime() /*return time in string format (ie: 09:28:32) */
{
static char time[20];
sprintf(time,"%02d:%02d:%02d",hour(),minute(),second());
return(time);
}
calc_time(sat_number) /* calculate the new realtime */
register sat_number;
{
if(dos_time) /* if in realtime, update time/date now */
{
settime();
}
realtime = floor(30.55 * (((double)month())+2.0)) - 2.0 * ( floor(.1 * (((double)month())+7.0))) - 91.0;
if(month() > 2)
{
if((((double)year())/4.0) == floor(((double)year())/4.0))
{
realtime += 1.0;
}
}
if(epoch_yr[sat_number] == year() - 1)
{
realtime += 365.0;
if(epoch_yr[sat_number]/4.0 == floor(epoch_yr[sat_number] / 4.0))
{
realtime += 1.0;
}
}
realtime = realtime + ((double)day()) + (((double)hour())/24.0) + (((double)minute())/1440.0) + (((double)second())/86400.0);
}
/* end of seesats.c */