#if HAS_FLIGHT_DEBUG
case ao_flight_test:
#if HAS_GYRO
- printf ("angle %4d pitch %7d yaw %7d roll %7d\n",
+ printf ("angle %4d pitch %7ld yaw %7ld roll %7ld\n",
ao_sample_orient,
((ao_sample_pitch << 9) - ao_ground_pitch) >> 9,
((ao_sample_yaw << 9) - ao_ground_yaw) >> 9,
printf ("sample:\n");
printf (" tick %d\n", ao_sample_tick);
#if HAS_BARO
- printf (" raw pres %d\n", ao_sample_pres);
+ printf (" raw pres %ld\n", ao_sample_pres);
#endif
#if HAS_ACCEL
printf (" raw accel %d\n", ao_sample_accel);
#endif
#if HAS_BARO
- printf (" ground pres %d\n", ao_ground_pres);
- printf (" ground alt %d\n", ao_ground_height);
+ printf (" ground pres %ld\n", ao_ground_pres);
+ printf (" ground alt %ld\n", ao_ground_height);
#endif
#if HAS_ACCEL
printf (" raw accel %d\n", ao_sample_accel);
#endif
#if HAS_BARO
- printf (" alt %d\n", ao_sample_alt);
- printf (" height %d\n", ao_sample_height);
+ printf (" alt %ld\n", ao_sample_alt);
+ printf (" height %ld\n", ao_sample_height);
#endif
#if HAS_ACCEL
printf ("kalman:\n");
- printf (" height %d\n", ao_height);
+ printf (" height %ld\n", ao_height);
printf (" speed %d.%02d\n", int_part(ao_speed), frac_part(ao_speed));
printf (" accel %d.%02d\n", int_part(ao_accel), frac_part(ao_accel));
- printf (" max_height %d\n", ao_max_height);
- printf (" avg_height %d\n", ao_avg_height);
- printf (" error_h %d\n", ao_error_h);
+ printf (" max_height %ld\n", ao_max_height);
+ printf (" avg_height %ld\n", ao_avg_height);
+ printf (" error_h %ld\n", ao_error_h);
#if !HAS_ACCEL
printf (" error_avg %d\n", ao_error_h_sq_avg);
#endif
ao_orient_test_select(void)
{
ao_orient_test = !ao_orient_test;
+ printf("orient test %d\n", ao_orient_test);
}
const struct ao_cmds ao_flight_cmds[] = {