diff options
-rw-r--r-- | ao.h | 2 | ||||
-rw-r--r-- | ao_monitor.c | 8 | ||||
-rw-r--r-- | ao_telemetry.c | 2 | ||||
-rw-r--r-- | aoview/aoview.h | 2 | ||||
-rw-r--r-- | aoview/aoview_monitor.c | 20 | ||||
-rw-r--r-- | aoview/aoview_state.c | 62 |
6 files changed, 42 insertions, 54 deletions
@@ -725,8 +725,10 @@ struct ao_telemetry { uint8_t addr; uint8_t flight_state; int16_t flight_accel; + int16_t ground_accel; int32_t flight_vel; int16_t flight_pres; + int16_t ground_pres; struct ao_adc adc; struct ao_gps_data gps; char callsign[AO_MAX_CALLSIGN]; diff --git a/ao_monitor.c b/ao_monitor.c index 880f257c..5997d427 100644 --- a/ao_monitor.c +++ b/ao_monitor.c @@ -36,12 +36,12 @@ ao_monitor(void) if (state > ao_flight_invalid) state = ao_flight_invalid; if (recv.status & PKT_APPEND_STATUS_1_CRC_OK) { - printf ("CALL %s SERIAL %3d RSSI %3d STATUS %02x STATE %7s ", + printf ("CALL %s SERIAL %3d RSSI %4d STATUS %02x STATE %7s ", callsign, recv.telemetry.addr, (int) recv.rssi - 74, recv.status, ao_state_names[state]); - printf("%5u a: %5d p: %5d t: %5d v: %5d d: %5d m: %5d fa: %5d fv: %7ld fp: %5d ", + printf("%5u a: %5d p: %5d t: %5d v: %5d d: %5d m: %5d fa: %5d ga: %d fv: %7ld fp: %5d gp: %5d ", recv.telemetry.adc.tick, recv.telemetry.adc.accel, recv.telemetry.adc.pres, @@ -50,8 +50,10 @@ ao_monitor(void) recv.telemetry.adc.sense_d, recv.telemetry.adc.sense_m, recv.telemetry.flight_accel, + recv.telemetry.ground_accel, recv.telemetry.flight_vel, - recv.telemetry.flight_pres); + recv.telemetry.flight_pres, + recv.telemetry.ground_pres); ao_gps_print(&recv.telemetry.gps); ao_rssi_set((int) recv.rssi - 74); } else { diff --git a/ao_telemetry.c b/ao_telemetry.c index b4461e92..5cf9ca61 100644 --- a/ao_telemetry.c +++ b/ao_telemetry.c @@ -37,8 +37,10 @@ ao_telemetry(void) ao_sleep(&ao_telemetry_interval); telemetry.flight_state = ao_flight_state; telemetry.flight_accel = ao_flight_accel; + telemetry.ground_accel = ao_ground_accel; telemetry.flight_vel = ao_flight_vel; telemetry.flight_pres = ao_flight_pres; + telemetry.ground_pres = ao_ground_pres; ao_adc_get(&telemetry.adc); ao_mutex_get(&ao_gps_mutex); memcpy(&telemetry.gps, &ao_gps_data, sizeof (struct ao_gps_data)); diff --git a/aoview/aoview.h b/aoview/aoview.h index 44412bec..4abbde88 100644 --- a/aoview/aoview.h +++ b/aoview/aoview.h @@ -59,8 +59,10 @@ struct aostate { int drogue; int main; int flight_accel; + int ground_accel; int flight_vel; int flight_pres; + int ground_pres; int nsat; int locked; struct { diff --git a/aoview/aoview_monitor.c b/aoview/aoview_monitor.c index b0189c60..7a04c82f 100644 --- a/aoview/aoview_monitor.c +++ b/aoview/aoview_monitor.c @@ -82,7 +82,7 @@ aoview_monitor_parse(char *line) if (words[nword] == NULL) break; } - if (nword < 32) + if (nword < 36) return; if (strcmp(words[0], "CALL") != 0) return; @@ -101,15 +101,17 @@ aoview_monitor_parse(char *line) aoview_parse_int(&state.drogue, words[20]); aoview_parse_int(&state.main, words[22]); aoview_parse_int(&state.flight_accel, words[24]); - aoview_parse_int(&state.flight_vel, words[26]); - aoview_parse_int(&state.flight_pres, words[28]); - aoview_parse_int(&state.nsat, words[30]); - if (strcmp (words[32], "unlocked") != 0 && nword >= 35) { + aoview_parse_int(&state.ground_accel, words[26]); + aoview_parse_int(&state.flight_vel, words[28]); + aoview_parse_int(&state.flight_pres, words[30]); + aoview_parse_int(&state.ground_pres, words[32]); + aoview_parse_int(&state.nsat, words[34]); + if (strcmp (words[36], "unlocked") != 0 && nword >= 41) { state.locked = 1; - sscanf(words[32], "%d:%d:%d", &state.gps_time.hour, &state.gps_time.minute, &state.gps_time.second); - aoview_parse_pos(&state.lat, words[33]); - aoview_parse_pos(&state.lon, words[34]); - sscanf(words[35], "%dm", &state.alt); + sscanf(words[36], "%d:%d:%d", &state.gps_time.hour, &state.gps_time.minute, &state.gps_time.second); + aoview_parse_pos(&state.lat, words[39]); + aoview_parse_pos(&state.lon, words[40]); + sscanf(words[41], "%dm", &state.alt); } else { state.locked = 0; state.gps_time.hour = state.gps_time.minute = state.gps_time.second = 0; diff --git a/aoview/aoview_state.c b/aoview/aoview_state.c index dda92af9..02ae0307 100644 --- a/aoview/aoview_state.c +++ b/aoview/aoview_state.c @@ -18,14 +18,9 @@ #include "aoview.h" #include <math.h> -static int pad_pres; -static int pad_accel; -static int pad_pres_total; -static int pad_accel_total; static double pad_lat_total; static double pad_lon_total; static int pad_alt_total; -static int npad; static int npad_gps; static int prev_tick; static double prev_accel; @@ -88,40 +83,28 @@ aoview_state_notify(struct aostate *state) double max_accel; if (!strcmp(state->state, "pad")) { - if (npad < NUM_PAD_SAMPLES) { - pad_accel_total += state->flight_accel; - pad_pres_total += state->flight_pres; - if (state->locked) { - pad_lat_total += state->lat; - pad_lon_total += state->lon; - pad_alt_total += state->alt; - npad_gps++; - } - npad++; + if (state->locked && npad_gps < NUM_PAD_SAMPLES) { + pad_lat_total += state->lat; + pad_lon_total += state->lon; + pad_alt_total += state->alt; + npad_gps++; } - if (npad <= NUM_PAD_SAMPLES) { - pad_pres = pad_pres_total / npad; - pad_accel = pad_accel_total / npad; - if (npad_gps) { - pad_lat = pad_lat_total / npad_gps; - pad_lon = pad_lon_total / npad_gps; - pad_alt = pad_alt_total / npad_gps; - } - } - if (npad == NUM_PAD_SAMPLES) { - npad++; - min_pres = pad_pres; - min_accel = pad_accel; + if (state->locked && npad_gps <= NUM_PAD_SAMPLES) { + pad_lat = pad_lat_total / npad_gps; + pad_lon = pad_lon_total / npad_gps; + pad_alt = pad_alt_total / npad_gps; } + min_pres = state->ground_pres; + min_accel = state->ground_accel; } if (state->flight_pres < min_pres) min_pres = state->flight_pres; if (state->flight_accel < min_accel) min_accel = state->flight_accel; - altitude = aoview_pres_to_altitude(state->flight_pres) - aoview_pres_to_altitude(pad_pres); - accel = (pad_accel - state->flight_accel) / 27.0; + altitude = aoview_pres_to_altitude(state->flight_pres) - aoview_pres_to_altitude(state->ground_pres); + accel = (state->ground_accel - state->flight_accel) / 27.0; velocity = state->flight_vel / 2700.0; - max_accel = (pad_accel - min_accel) / 27.0; + max_accel = (state->ground_accel - min_accel) / 27.0; ticks = state->tick - prev_tick; temp = ((state->temp / 32767.0 * 3.3) - 0.5) / 0.01; battery = (state->batt / 32767.0 * 5.0); @@ -132,20 +115,20 @@ aoview_state_notify(struct aostate *state) prev_tick = state->tick; aoview_table_start(); - if (npad >= NUM_PAD_SAMPLES) + if (npad_gps >= NUM_PAD_SAMPLES) aoview_table_add_row("Ground state", "ready"); else - aoview_table_add_row("Ground state", "preparing (%d)", - NUM_PAD_SAMPLES - npad); + aoview_table_add_row("Ground state", "waiting for gps (%d)", + NUM_PAD_SAMPLES - npad_gps); aoview_table_add_row("Rocket state", "%s", state->state); aoview_table_add_row("Callsign", "%s", state->callsign); aoview_table_add_row("Rocket serial", "%d", state->serial); - aoview_table_add_row("RSSI", "%ddB", state->rssi); + aoview_table_add_row("RSSI", "%ddBm", state->rssi); aoview_table_add_row("Height", "%dm", altitude); aoview_table_add_row("Max height", "%dm", aoview_pres_to_altitude(min_pres) - - aoview_pres_to_altitude(pad_pres)); + aoview_pres_to_altitude(state->ground_pres)); aoview_table_add_row("Acceleration", "%gm/s²", accel); aoview_table_add_row("Max acceleration", "%gm/s²", max_accel); aoview_table_add_row("Velocity", "%gm/s", velocity); @@ -153,7 +136,7 @@ aoview_state_notify(struct aostate *state) aoview_table_add_row("Battery", "%gV", battery); aoview_table_add_row("Drogue", "%gV", drogue_sense); aoview_table_add_row("Main", "%gV", main_sense); - aoview_table_add_row("Pad altitude", "%dm", aoview_pres_to_altitude(pad_pres)); + aoview_table_add_row("Pad altitude", "%dm", aoview_pres_to_altitude(state->ground_pres)); aoview_table_add_row("Satellites", "%d", state->nsat); if (state->locked) { aoview_state_add_deg("Latitude", state->lat); @@ -181,14 +164,9 @@ aoview_state_notify(struct aostate *state) void aoview_state_new(void) { - pad_pres = 0; - pad_accel = 0; - pad_pres_total = 0; - pad_accel_total = 0; pad_lat_total = 0; pad_lon_total = 0; pad_alt_total = 0; - npad = 0; npad_gps = 0; prev_tick = 0; prev_accel = 0; |