/contrib/ntp/ntpd/jupiter.h
https://bitbucket.org/freebsd/freebsd-head/ · C++ Header · 255 lines · 216 code · 18 blank · 21 comment · 0 complexity · de4be677a0fa4862a40f6f14bb17a9af MD5 · raw file
- /* @(#) $Header$ (LBL) */
- /*
- * Rockwell Jupiter GPS receiver definitions
- *
- * This is all based on the "Zodiac GPS Receiver Family Designer's
- * Guide" (dated 12/96)
- */
- #define JUPITER_SYNC 0x81ff /* sync word (book says 0xff81 !?!?) */
- #define JUPITER_ALL 0xffff /* disable all output messages */
- /* Output messages (sent by the Jupiter board) */
- #define JUPITER_O_GPOS 1000 /* geodetic position status */
- #define JUPITER_O_EPOS 1001 /* ECEF position status */
- #define JUPITER_O_CHAN 1002 /* channel summary */
- #define JUPITER_O_VIS 1003 /* visible satellites */
- #define JUPITER_O_DGPS 1005 /* differential GPS status */
- #define JUPITER_O_MEAS 1007 /* channel measurement */
- #define JUPITER_O_ID 1011 /* receiver id */
- #define JUPITER_O_USER 1012 /* user-settings output */
- #define JUPITER_O_TEST 1100 /* built-in test results */
- #define JUPITER_O_MARK 1102 /* measurement time mark */
- #define JUPITER_O_PULSE 1108 /* UTC time mark pulse output */
- #define JUPITER_O_PORT 1130 /* serial port com parameters in use */
- #define JUPITER_O_EUP 1135 /* EEPROM update */
- #define JUPITER_O_ESTAT 1136 /* EEPROM status */
- /* Input messages (sent to the Jupiter board) */
- #define JUPITER_I_PVTINIT 1200 /* geodetic position and velocity */
- #define JUPITER_I_USER 1210 /* user-defined datum */
- #define JUPITER_I_MAPSEL 1211 /* map datum select */
- #define JUPITER_I_ELEV 1212 /* satellite elevation mask control */
- #define JUPITER_I_CAND 1213 /* satellite candidate select */
- #define JUPITER_I_DGPS 1214 /* differential GPS control */
- #define JUPITER_I_COLD 1216 /* cold start control */
- #define JUPITER_I_VALID 1217 /* solution validity criteria */
- #define JUPITER_I_ALT 1219 /* user-entered altitude input */
- #define JUPITER_I_PLAT 1220 /* application platform control */
- #define JUPITER_I_NAV 1221 /* nav configuration */
- #define JUPITER_I_TEST 1300 /* preform built-in test command */
- #define JUPITER_I_RESTART 1303 /* restart command */
- #define JUPITER_I_PORT 1330 /* serial port com parameters */
- #define JUPITER_I_PROTO 1331 /* message protocol control */
- #define JUPITER_I_RDGPS 1351 /* raw DGPS RTCM SC-104 data */
- struct jheader {
- u_short sync; /* (JUPITER_SYNC) */
- u_short id; /* message id */
- u_short len; /* number of data short wordss (w/o cksum) */
- u_char reqid; /* JUPITER_REQID_MASK bits available as id */
- u_char flags; /* flags */
- u_short hsum; /* header cksum */
- };
- #define JUPITER_REQID_MASK 0x3f /* bits available as id */
- #define JUPITER_FLAG_NAK 0x01 /* negative acknowledgement */
- #define JUPITER_FLAG_ACK 0x02 /* acknowledgement */
- #define JUPITER_FLAG_REQUEST 0x04 /* request ACK or NAK */
- #define JUPITER_FLAG_QUERY 0x08 /* request one shot output message */
- #define JUPITER_FLAG_LOG 0x20 /* request periodic output message */
- #define JUPITER_FLAG_CONN 0x40 /* enable periodic message */
- #define JUPITER_FLAG_DISC 0x80 /* disable periodic message */
- #define JUPITER_H_FLAG_BITS \
- "\020\1NAK\2ACK\3REQUEST\4QUERY\5MBZ\6LOG\7CONN\10DISC"
- /* Log request messages (data payload when using JUPITER_FLAG_LOG) */
- struct jrequest {
- u_short trigger; /* if 0, trigger on time trigger on
- update (e.g. new almanac) */
- u_short interval; /* frequency in seconds */
- u_short offset; /* offset into minute */
- u_short dsum; /* checksum */
- };
- /* JUPITER_O_GPOS (1000) */
- struct jgpos {
- u_short stime[2]; /* set time (10 ms ticks) */
- u_short seq; /* sequence number */
- u_short sseq; /* sat measurement sequence number */
- u_short navval; /* navigation soltuion validity */
- u_short navtype; /* navigation solution type */
- u_short nmeas; /* # of measurements used in solution */
- u_short polar; /* if 1 then polar navigation */
- u_short gweek; /* GPS week number */
- u_short sweek[2]; /* GPS seconds into week */
- u_short nsweek[2]; /* GPS nanoseconds into second */
- u_short utcday; /* 1 to 31 */
- u_short utcmon; /* 1 to 12 */
- u_short utcyear; /* 1980 to 2079 */
- u_short utchour; /* 0 to 23 */
- u_short utcmin; /* 0 to 59 */
- u_short utcsec; /* 0 to 59 */
- u_short utcnsec[2]; /* 0 to 999999999 */
- u_short lat[2]; /* latitude (radians) */
- u_short lon[2]; /* longitude (radians) */
- u_short height[2]; /* height (meters) */
- u_short gsep; /* geoidal separation */
- u_short speed[2]; /* ground speed (meters/sec) */
- u_short course; /* true course (radians) */
- u_short mvar;
- u_short climb;
- u_short mapd;
- u_short herr[2];
- u_short verr[2];
- u_short terr[2];
- u_short hverr;
- u_short bias[2];
- u_short biassd[2];
- u_short drift[2];
- u_short driftsd[2];
- u_short dsum; /* checksum */
- };
- #define JUPITER_O_GPOS_NAV_NOALT 0x01 /* altitude used */
- #define JUPITER_O_GPOS_NAV_NODGPS 0x02 /* no differential GPS */
- #define JUPITER_O_GPOS_NAV_NOSAT 0x04 /* not enough satellites */
- #define JUPITER_O_GPOS_NAV_MAXH 0x08 /* exceeded max EHPE */
- #define JUPITER_O_GPOS_NAV_MAXV 0x10 /* exceeded max EVPE */
- /* JUPITER_O_CHAN (1002) */
- struct jchan {
- u_short stime[2]; /* set time (10 ms ticks) */
- u_short seq; /* sequence number */
- u_short sseq; /* sat measurement sequence number */
- u_short gweek; /* GPS week number */
- u_short sweek[2]; /* GPS seconds into week */
- u_short gpsns[2]; /* GPS nanoseconds from epoch */
- struct jchan2 {
- u_short flags; /* flags */
- u_short prn; /* satellite PRN */
- u_short chan; /* channel number */
- } sat[12];
- u_short dsum;
- };
- /* JUPITER_O_VIS (1003) */
- struct jvis {
- u_short stime[2]; /* set time (10 ms ticks) */
- u_short seq; /* sequence number */
- u_short gdop; /* best possible GDOP */
- u_short pdop; /* best possible PDOP */
- u_short hdop; /* best possible HDOP */
- u_short vdop; /* best possible VDOP */
- u_short tdop; /* best possible TDOP */
- u_short nvis; /* number of visible satellites */
- struct jvis2 {
- u_short prn; /* satellite PRN */
- u_short azi; /* satellite azimuth (radians) */
- u_short elev; /* satellite elevation (radians) */
- } sat[12];
- u_short dsum; /* checksum */
- };
- /* JUPITER_O_ID (1011) */
- struct jid {
- u_short stime[2]; /* set time (10 ms ticks) */
- u_short seq; /* sequence number */
- char chans[20]; /* number of channels (ascii) */
- char vers[20]; /* software version (ascii) */
- char date[20]; /* software date (ascii) */
- char opts[20]; /* software options (ascii) */
- char reserved[20];
- u_short dsum; /* checksum */
- };
- /* JUPITER_O_USER (1012) */
- struct juser {
- u_short stime[2]; /* set time (10 ms ticks) */
- u_short seq; /* sequence number */
- u_short status; /* operatinoal status */
- u_short coldtmo; /* cold start time-out */
- u_short dgpstmo; /* DGPS correction time-out*/
- u_short emask; /* elevation mask */
- u_short selcand[2]; /* selected candidate */
- u_short solflags; /* solution validity criteria */
- u_short nsat; /* number of satellites in track */
- u_short herr[2]; /* minimum expected horizontal error */
- u_short verr[2]; /* minimum expected vertical error */
- u_short platform; /* application platform */
- u_short dsum; /* checksum */
- };
- /* JUPITER_O_PULSE (1108) */
- struct jpulse {
- u_short stime[2]; /* set time (10 ms ticks) */
- u_short seq; /* sequence number */
- u_short reserved[5];
- u_short sweek[2]; /* GPS seconds into week */
- short offs; /* GPS to UTC time offset (seconds) */
- u_short offns[2]; /* GPS to UTC offset (nanoseconds) */
- u_short flags; /* flags */
- u_short dsum; /* checksum */
- };
- #define JUPITER_O_PULSE_VALID 0x1 /* time mark validity */
- #define JUPITER_O_PULSE_UTC 0x2 /* GPS/UTC sync */
- /* JUPITER_O_EUP (1135) */
- struct jeup {
- u_short stime[2]; /* set time (10 ms ticks) */
- u_short seq; /* sequence number */
- u_char dataid; /* data id */
- u_char prn; /* satellite PRN */
- u_short dsum; /* checksum */
- };
- /* JUPITER_I_RESTART (1303) */
- struct jrestart {
- u_short seq; /* sequence number */
- u_short flags;
- u_short dsum; /* checksum */
- };
- #define JUPITER_I_RESTART_INVRAM 0x01
- #define JUPITER_I_RESTART_INVEEPROM 0x02
- #define JUPITER_I_RESTART_INVRTC 0x04
- #define JUPITER_I_RESTART_COLD 0x80
- /* JUPITER_I_PVTINIT (1200) */
- struct jpvtinit {
- u_short flags;
- u_short gweek; /* GPS week number */
- u_short sweek[2]; /* GPS seconds into week */
- u_short utcday; /* 1 to 31 */
- u_short utcmon; /* 1 to 12 */
- u_short utcyear; /* 1980 to 2079 */
- u_short utchour; /* 0 to 23 */
- u_short utcmin; /* 0 to 59 */
- u_short utcsec; /* 0 to 59 */
- u_short lat[2]; /* latitude (radians) */
- u_short lon[2]; /* longitude (radians) */
- u_short height[2]; /* height (meters) */
- u_short speed[2]; /* ground speed (meters/sec) */
- u_short course; /* true course (radians) */
- u_short climb;
- u_short dsum;
- };
- #define JUPITER_I_PVTINIT_FORCE 0x01
- #define JUPITER_I_PVTINIT_GPSVAL 0x02
- #define JUPITER_I_PVTINIT_UTCVAL 0x04
- #define JUPITER_I_PVTINIT_POSVAL 0x08
- #define JUPITER_I_PVTINIT_ALTVAL 0x10
- #define JUPITER_I_PVTINIT_SPDVAL 0x12
- #define JUPITER_I_PVTINIT_MAGVAL 0x14
- #define JUPITER_I_PVTINIT_CLIMBVAL 0x18
- /* JUPITER_I_PLAT (1220) */
- struct jplat {
- u_short seq; /* sequence number */
- u_short platform; /* application platform */
- u_short dsum;
- };
- #define JUPITER_I_PLAT_DEFAULT 0 /* default dynamics */
- #define JUPITER_I_PLAT_LOW 2 /* pedestrian */
- #define JUPITER_I_PLAT_MED 5 /* land (e.g. automobile) */
- #define JUPITER_I_PLAT_HIGH 6 /* air */