X-Git-Url: https://git.gag.com/?p=fw%2Faltos;a=blobdiff_plain;f=ao-tools%2Flib%2Fcc-telemetry.h;h=d64c4b30d3d0395cc6ce593d675dfc1ed0fa20b3;hp=5a66b971df0e032987c27823cb062e311a4b9ce6;hb=f6d633d73a8f826cf2a3128e3e234bd11af49718;hpb=82604193ed0c522c1fba0072b504fe88b027f1ee

diff --git a/ao-tools/lib/cc-telemetry.h b/ao-tools/lib/cc-telemetry.h
index 5a66b971..d64c4b30 100644
--- a/ao-tools/lib/cc-telemetry.h
+++ b/ao-tools/lib/cc-telemetry.h
@@ -29,7 +29,9 @@ struct ao_telemetry_generic {
 	uint16_t	tick;		/* 2 */
 	uint8_t		type;		/* 4 */
 	uint8_t		payload[27];	/* 5 */
-	/* 32 */
+	uint8_t		rssi;		/* 32 */
+	uint8_t		status;		/* 33 */
+	/* 34 */
 };
 
 #define AO_TELEMETRY_SENSOR_TELEMETRUM	0x01
@@ -148,6 +150,123 @@ struct ao_telemetry_companion {
 	/* 32 */
 };
 	
+#define AO_TELEMETRY_MEGA_SENSOR	0x08
+
+struct ao_telemetry_mega_sensor {
+	uint16_t	serial;		/*  0 */
+	uint16_t	tick;		/*  2 */
+	uint8_t		type;		/*  4 */
+
+	uint8_t		orient;		/*  5 angle from vertical */
+	int16_t		accel;		/*  6 Z axis */
+
+	int32_t		pres;		/*  8 Pa * 10 */
+	int16_t		temp;		/* 12 °C * 100 */
+
+	int16_t		accel_x;	/* 14 */
+	int16_t		accel_y;	/* 16 */
+	int16_t		accel_z;	/* 18 */
+
+	int16_t		gyro_x;		/* 20 */
+	int16_t		gyro_y;		/* 22 */
+	int16_t		gyro_z;		/* 24 */
+
+	int16_t		mag_x;		/* 26 */
+	int16_t		mag_y;		/* 28 */
+	int16_t		mag_z;		/* 30 */
+	/* 32 */
+};
+	
+#define AO_TELEMETRY_MEGA_DATA		0x09
+
+struct ao_telemetry_mega_data {
+	uint16_t	serial;		/*  0 */
+	uint16_t	tick;		/*  2 */
+	uint8_t		type;		/*  4 */
+
+	uint8_t         state;          /*  5 flight state */
+
+	int16_t		v_batt;		/*  6 battery voltage */
+	int16_t		v_pyro;		/*  8 pyro battery voltage */
+	int8_t		sense[6];	/* 10 continuity sense */
+
+	int32_t		ground_pres;	/* 16 average pres on pad */
+	int16_t		ground_accel;	/* 20 average accel on pad */
+	int16_t		accel_plus_g;	/* 22 accel calibration at +1g */
+	int16_t		accel_minus_g;	/* 24 accel calibration at -1g */
+
+	int16_t         acceleration;   /* 26 m/s² * 16 */
+	int16_t         speed;          /* 28 m/s * 16 */
+	int16_t         height;         /* 30 m */
+	/* 32 */
+};
+
+#define AO_TELEMETRY_METRUM_SENSOR	0x0A
+
+struct ao_telemetry_metrum_sensor {
+	uint16_t	serial;		/*  0 */
+	uint16_t	tick;		/*  2 */
+	uint8_t		type;		/*  4 */
+
+	uint8_t         state;          /*  5 flight state */
+	int16_t		accel;		/*  6 Z axis */
+
+	int32_t		pres;		/*  8 Pa * 10 */
+	int16_t		temp;		/* 12 °C * 100 */
+
+	int16_t         acceleration;   /* 14 m/s² * 16 */
+	int16_t         speed;          /* 16 m/s * 16 */
+	int16_t         height;         /* 18 m */
+
+	int16_t		v_batt;		/* 20 battery voltage */
+	int16_t		sense_a;	/* 22 apogee continuity sense */
+	int16_t		sense_m;	/* 24 main continuity sense */
+
+	uint8_t		pad[6];		/* 26 */
+	/* 32 */
+};
+	
+#define AO_TELEMETRY_METRUM_DATA	0x0B
+
+struct ao_telemetry_metrum_data {
+	uint16_t	serial;		/*  0 */
+	uint16_t	tick;		/*  2 */
+	uint8_t		type;		/*  4 */
+
+	int32_t		ground_pres;	/* 8 average pres on pad */
+	int16_t		ground_accel;	/* 12 average accel on pad */
+	int16_t		accel_plus_g;	/* 14 accel calibration at +1g */
+	int16_t		accel_minus_g;	/* 16 accel calibration at -1g */
+
+	uint8_t		pad[14];	/* 18 */
+	/* 32 */
+};
+
+#define AO_TELEMETRY_MINI		0x10
+
+struct ao_telemetry_mini {
+	uint16_t	serial;		/*  0 */
+	uint16_t	tick;		/*  2 */
+	uint8_t		type;		/*  4 */
+
+	uint8_t         state;          /*  5 flight state */
+	int16_t		v_batt;		/*  6 battery voltage */
+	int16_t		sense_a;	/*  8 apogee continuity */
+	int16_t		sense_m;	/* 10 main continuity */
+
+	int32_t		pres;		/* 12 Pa * 10 */
+	int16_t		temp;		/* 16 °C * 100 */
+
+	int16_t         acceleration;   /* 18 m/s² * 16 */
+	int16_t         speed;          /* 20 m/s * 16 */
+	int16_t         height;         /* 22 m */
+
+	int32_t		ground_pres;	/* 24 average pres on pad */
+
+	int32_t		pad28;		/* 28 */
+	/* 32 */
+};
+
 /* #define AO_SEND_ALL_BARO */
 
 #define AO_TELEMETRY_BARO		0x80
@@ -179,10 +298,27 @@ union ao_telemetry_all {
 	struct ao_telemetry_location		location;
 	struct ao_telemetry_satellite		satellite;
 	struct ao_telemetry_companion		companion;
+	struct ao_telemetry_mega_sensor		mega_sensor;
+	struct ao_telemetry_mega_data		mega_data;
+	struct ao_telemetry_metrum_sensor	metrum_sensor;
+	struct ao_telemetry_metrum_data		metrum_data;
+	struct ao_telemetry_mini		mini;
 	struct ao_telemetry_baro		baro;
 };
 
+#define CC_TELEMETRY_HEADER	"TELEM"
+
+/* "TELEM " 1 byte length 32 data bytes 1 rssi 1 status 1 checksum 1 null */
+
+#define CC_TELEMETRY_BUFSIZE	(6 + (1 + 32 + 3) * 2 + 1)
+
 int
 cc_telemetry_parse(const char *input_line, union ao_telemetry_all *telemetry);
 
+uint8_t
+cc_telemetry_cksum(const union ao_telemetry_all *telemetry);
+
+void
+cc_telemetry_unparse(const union ao_telemetry_all *telemetry, char output_line[CC_TELEMETRY_BUFSIZE]);
+
 #endif