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/* @(#) $Header$ (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 */
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