X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=src%2Fkernel%2Fao_sample.c;h=2c77c36920ed5755046e158c9e32f4e92e2d9aae;hb=3ed101d634968666cd3ee2d8c49737970caf406b;hp=46771496b69a4745cd6ea24597f9fa048c7243ba;hpb=4370b7e7bc48d3f3f3ec94665449f1fde4e9567c;p=fw%2Faltos diff --git a/src/kernel/ao_sample.c b/src/kernel/ao_sample.c index 46771496..2c77c369 100644 --- a/src/kernel/ao_sample.c +++ b/src/kernel/ao_sample.c @@ -57,6 +57,9 @@ angle_t ao_sample_orient; angle_t ao_sample_orients[AO_NUM_ORIENT]; uint8_t ao_sample_orient_pos; #endif +#ifdef HAS_MOTOR_PRESSURE +motor_pressure_t ao_sample_motor_pressure; +#endif uint8_t ao_sample_data; @@ -87,6 +90,10 @@ int32_t ao_ground_yaw; int32_t ao_ground_roll; #endif +#if HAS_MOTOR_PRESSURE +motor_pressure_t ao_ground_motor_pressure; +#endif + static uint8_t ao_preflight; /* in preflight mode */ static uint16_t nsamples; @@ -107,6 +114,9 @@ int32_t ao_sample_yaw_sum; int32_t ao_sample_roll_sum; static struct ao_quaternion ao_rotation; #endif +#if HAS_MOTOR_PRESSURE +int32_t ao_sample_motor_pressure_sum; +#endif #if HAS_FLIGHT_DEBUG extern uint8_t ao_orient_test; @@ -130,6 +140,9 @@ ao_sample_preflight_add(void) ao_sample_pitch_sum += ao_sample_pitch; ao_sample_yaw_sum += ao_sample_yaw; ao_sample_roll_sum += ao_sample_roll; +#endif +#if HAS_MOTOR_PRESSURE + ao_sample_motor_pressure_sum += ao_sample_motor_pressure; #endif ++nsamples; } @@ -197,15 +210,18 @@ ao_sample_preflight_set(void) ao_ground_accel_along = ao_sample_accel_along_sum >> 9; ao_ground_accel_across = ao_sample_accel_across_sum >> 9; ao_ground_accel_through = ao_sample_accel_through_sum >> 9; - + ao_sample_accel_along_sum = 0; + ao_sample_accel_across_sum = 0; + ao_sample_accel_through_sum = 0; +#endif +#if HAS_MOTOR_PRESSURE + ao_ground_motor_pressure = ao_sample_motor_pressure_sum >> 9; + ao_sample_motor_pressure_sum = 0; #endif #if HAS_GYRO ao_ground_pitch = ao_sample_pitch_sum; ao_ground_yaw = ao_sample_yaw_sum; ao_ground_roll = ao_sample_roll_sum; - ao_sample_accel_along_sum = 0; - ao_sample_accel_across_sum = 0; - ao_sample_accel_through_sum = 0; ao_sample_pitch_sum = 0; ao_sample_yaw_sum = 0; ao_sample_roll_sum = 0; @@ -241,7 +257,7 @@ ao_sample_preflight_set(void) (ao_ground_accel_across - ao_config.accel_zero_across), (ao_ground_accel_through - ao_config.accel_zero_through), (ao_ground_accel_along - ao_config.accel_zero_along)); -#endif +#endif ao_sample_compute_orient(); ao_sample_set_all_orients(); @@ -379,6 +395,9 @@ ao_sample(void) ao_sample_yaw = ao_data_yaw(ao_data); ao_sample_roll = ao_data_roll(ao_data); #endif +#if HAS_MOTOR_PRESSURE + ao_sample_motor_pressure = ao_data_motor_pressure(ao_data); +#endif if (ao_preflight) ao_sample_preflight();