summaryrefslogtreecommitdiff
diff options
context:
space:
mode:
authorKeith Packard <keithp@keithp.com>2011-06-24 08:31:51 -0700
committerKeith Packard <keithp@keithp.com>2011-06-27 19:16:42 -0700
commit336224a08327cadc95f6e5b564a4ddc64aaad8f8 (patch)
treeb60cd78f9adf034457b2962fc9381865b48caa86
parent5e111fdf1f23203baeeb490ae1b69402ebd513b8 (diff)
altos: Start adding new telemetry frame definitions
These use the initial 24 bytes per frame plan, which will probably get changed to 32 bytes per frame. Signed-off-by: Keith Packard <keithp@keithp.com>
-rw-r--r--src/ao.h89
1 files changed, 89 insertions, 0 deletions
diff --git a/src/ao.h b/src/ao.h
index f5753703..4895f016 100644
--- a/src/ao.h
+++ b/src/ao.h
@@ -1042,6 +1042,95 @@ ao_gps_report_init(void);
#define AO_MAX_CALLSIGN 8
#define AO_MAX_TELEMETRY 128
+struct ao_telemetry_generic {
+ uint16_t serial; /* 0 */
+ uint16_t tick; /* 2 */
+ uint8_t type; /* 4 */
+ uint8_t payload[19]; /* 5 */
+ /* 24 */
+};
+
+#define AO_TELEMETRY_SENSOR_TELEMETRUM 0x01
+#define AO_TELEMETRY_SENSOR_TELEMINI 0x02
+#define AO_TELEMETRY_SENSOR_TELENANO 0x03
+
+struct ao_telemetry_sensor {
+ uint16_t serial; /* 0 */
+ uint16_t tick; /* 2 */
+ uint8_t type; /* 4 */
+
+ uint8_t state; /* 5 flight state */
+ int16_t accel; /* 6 accelerometer (TM only) */
+ int16_t pres; /* 8 pressure sensor */
+ int16_t temp; /* 10 temperature sensor */
+ int16_t v_batt; /* 12 battery voltage */
+ int16_t sense_d; /* 14 drogue continuity sense (TM/Tm) */
+ int16_t sense_m; /* 16 main continuity sense (TM/Tm) */
+
+ int16_t acceleration; /* 18 m/s² * 16 */
+ int16_t speed; /* 20 m/s * 16 */
+ int16_t height; /* 22 m */
+ /* 24 */
+};
+
+#define AO_TELEMETRY_CONSTANT 0x10
+
+struct ao_telemetry_constant {
+ uint16_t serial; /* 0 */
+ uint16_t tick; /* 2 */
+ uint8_t type; /* 4 */
+ uint8_t device; /* 5 device type */
+ uint16_t flight; /* 6 flight number */
+ int16_t ground_accel; /* 8 average ground accelerometer (TM only) */
+ int16_t ground_pres; /* 10 average ground barometer */
+ int16_t accel_plus_g; /* 12 +1g accelerometer calibration value (TM only) */
+ int16_t accel_minus_g; /* 14 -1g accelermeter calibration value (TM only) */
+ char callsign[AO_MAX_CALLSIGN]; /* 16 identity */
+ /* 24 */
+};
+
+#define AO_TELEMETRY_LOCATION 0x11
+
+struct ao_telemetry_location {
+ uint16_t serial; /* 0 */
+ uint16_t tick; /* 2 */
+ uint8_t type; /* 4 */
+ uint8_t flags; /* 5 Number of sats and other flags */
+ int16_t altitude; /* 6 GPS reported altitude (m) */
+ int32_t latitude; /* 8 latitude (degrees * 10⁷) */
+ int32_t longitude; /* 12 longitude (degrees * 10⁷) */
+ uint8_t year; /* 16 (- 2000) */
+ uint8_t month; /* 17 (1-12) */
+ uint8_t day; /* 18 (1-31) */
+ uint8_t hour; /* 19 (0-23) */
+ uint8_t minute; /* 20 (0-59) */
+ uint8_t second; /* 21 (0-59) */
+ uint8_t hdop; /* 22 (m * 5) */
+ uint8_t unused; /* 23 */
+ /* 24 */
+};
+
+#define AO_TELEMETRY_SATELLITE 0x12
+
+struct ao_telemetry_satellite {
+ uint16_t serial; /* 0 */
+ uint16_t tick; /* 2 */
+ uint8_t type; /* 4 */
+ uint8_t channels; /* 5 number of reported sats */
+ uint8_t sats_0_1[3]; /* 6 reported sats 0 and 1 */
+ uint8_t sats_2_3[3];
+ uint8_t sats_4_5[3];
+ uint8_t sats_6_7[3];
+ uint8_t sats_8_9[3];
+ uint8_t sats_10_11[3];
+ /* 24 */
+};
+
+#define AO_SAT_0_SSID(s) ((s)[0] & 0x3f)
+#define AO_SAT_0_C_N_1(s) ((((s)[0] & 0xc0) >> 2) | ((s)[1] & 0x0f))
+#define AO_SAT_1_SSID(s) ((((s)[1] & 0xf0) >> 2) | ((s)[2] & 0x03))
+#define AO_SAT_1_C_N_1(s) (((s)[2] & 0xfc) >> 2)
+
struct ao_telemetry_orig {
uint16_t serial;
uint16_t flight;