X-Git-Url: https://git.gag.com/?p=fw%2Faltos;a=blobdiff_plain;f=src%2Fcore%2Fao_flight.c;h=88dc816d25578858aa2c3e8c672cb414b0eb418e;hp=39084fd0fa2cad5d2078a45a0ac1231cfd05108f;hb=4254de22864de2ed7ae5928c6b8bfd9df1c8a3fb;hpb=6694cedd560a7ea9520ef11472c2770b489187c0 diff --git a/src/core/ao_flight.c b/src/core/ao_flight.c index 39084fd0..88dc816d 100644 --- a/src/core/ao_flight.c +++ b/src/core/ao_flight.c @@ -40,6 +40,7 @@ __pdata enum ao_flight_state ao_flight_state; /* current flight state */ __pdata uint16_t ao_boost_tick; /* time of launch detect */ +__pdata uint16_t ao_motor_number; /* number of motors burned so far */ /* * track min/max data over a long interval to detect @@ -93,7 +94,9 @@ ao_flight(void) if (ao_config.accel_plus_g == 0 || ao_config.accel_minus_g == 0 || ao_ground_accel < ao_config.accel_plus_g - ACCEL_NOSE_UP || - ao_ground_accel > ao_config.accel_minus_g + ACCEL_NOSE_UP) + ao_ground_accel > ao_config.accel_minus_g + ACCEL_NOSE_UP || + ao_ground_height < -1000 || + ao_ground_height > 7000) { /* Detected an accel value outside -1.5g to 1.5g * (or uncalibrated values), so we go into invalid mode @@ -114,14 +117,14 @@ ao_flight(void) { /* Set pad mode - we can fly! */ ao_flight_state = ao_flight_pad; -#if HAS_USB && HAS_RADIO +#if HAS_USB && !HAS_FLIGHT_DEBUG && !HAS_SAMPLE_PROFILE /* Disable the USB controller in flight mode * to save power */ ao_usb_disable(); #endif -#if !HAS_ACCEL +#if !HAS_ACCEL && PACKET_HAS_SLAVE /* Disable packet mode in pad state on TeleMini */ ao_packet_slave_stop(); #endif @@ -131,8 +134,10 @@ ao_flight(void) ao_rdf_set(1); ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_PAD); #endif +#if HAS_LED /* signal successful initialization by turning off the LED */ ao_led_off(AO_LED_RED); +#endif } else { /* Set idle mode */ ao_flight_state = ao_flight_idle; @@ -142,8 +147,10 @@ ao_flight(void) ao_packet_slave_start(); #endif +#if HAS_LED /* signal successful initialization by turning off the LED */ ao_led_off(AO_LED_RED); +#endif } /* wakeup threads due to state change */ ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); @@ -215,6 +222,7 @@ ao_flight(void) #else ao_flight_state = ao_flight_coast; #endif + ++ao_motor_number; ao_wakeup(DATA_TO_XDATA(&ao_flight_state)); } break; @@ -358,7 +366,7 @@ ao_flight(void) } } -#if !HAS_RADIO +#if HAS_FLIGHT_DEBUG static inline int int_part(int16_t i) { return i >> 4; } static inline int frac_part(int16_t i) { return ((i & 0xf) * 100 + 8) / 16; } @@ -378,6 +386,7 @@ ao_flight_dump(void) printf (" raw accel %d\n", ao_sample_accel); #endif printf (" ground pres %d\n", ao_ground_pres); + printf (" ground alt %d\n", ao_ground_height); #if HAS_ACCEL printf (" raw accel %d\n", ao_sample_accel); printf (" groundaccel %d\n", ao_ground_accel); @@ -413,7 +422,7 @@ void ao_flight_init(void) { ao_flight_state = ao_flight_startup; -#if !HAS_RADIO +#if HAS_FLIGHT_DEBUG ao_cmd_register(&ao_flight_cmds[0]); #endif ao_add_task(&flight_task, ao_flight, "flight");