__pdata gyro_t ao_sample_roll;
__pdata gyro_t ao_sample_pitch;
__pdata gyro_t ao_sample_yaw;
-__pdata angle_t ao_orient;
+__pdata angle_t ao_sample_orient;
#endif
__data uint8_t ao_sample_data;
__pdata accel_t ao_ground_accel_along;
__pdata accel_t ao_ground_accel_across;
__pdata accel_t ao_ground_accel_through;
-__pdata gyro_t ao_ground_pitch;
-__pdata gyro_t ao_ground_yaw;
-__pdata gyro_t ao_ground_roll;
+__pdata int32_t ao_ground_pitch;
+__pdata int32_t ao_ground_yaw;
+__pdata int32_t ao_ground_roll;
#endif
static __pdata uint8_t ao_preflight; /* in preflight mode */
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_ground_pitch = ao_sample_pitch_sum >> 9;
- ao_ground_yaw = ao_sample_yaw_sum >> 9;
- ao_ground_roll = ao_sample_roll_sum >> 9;
+ 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;
- ao_orient = 0;
+ ao_sample_orient = 0;
/* No rotation yet */
ao_quaternion_init_zero_rotation(&ao_rotation);
- /* XXX Assume we're pointing straight up for now */
+ /* Take the pad IMU acceleration values and compute our current direction
+ */
ao_quaternion_init_vector(&ao_pad_orientation,
- ao_ground_accel_across,
- ao_ground_accel_through,
- -ao_ground_accel_along);
+ 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);
+
ao_quaternion_normalize(&ao_pad_orientation,
&ao_pad_orientation);
- printf ("pad r%8.5f x%8.5f y%8.5f z%8.5f\n",
- ao_pad_orientation.r,
- ao_pad_orientation.x,
- ao_pad_orientation.y,
- ao_pad_orientation.z);
#endif
nsamples = 0;
}
#else
static const float dt = 1/100.0;
#endif
- float x = ao_mpu6000_gyro(ao_sample_pitch - ao_ground_pitch) * dt;
- float y = ao_mpu6000_gyro(ao_sample_yaw - ao_ground_yaw) * dt;
- float z = ao_mpu6000_gyro(ao_sample_roll - ao_ground_roll) * dt;
-
- float n_2, n;
- float s, c;
-
+ float x = ao_mpu6000_gyro((float) ((ao_sample_pitch << 9) - ao_ground_pitch) / 512.0f) * dt;
+ float y = ao_mpu6000_gyro((float) ((ao_sample_yaw << 9) - ao_ground_yaw) / 512.0f) * dt;
+ float z = ao_mpu6000_gyro((float) ((ao_sample_roll << 9) - ao_ground_roll) / 512.0f) * dt;
struct ao_quaternion rot;
struct ao_quaternion point;
ao_quaternion_rotate(&point, &ao_pad_orientation, &ao_rotation);
- ao_orient = acosf(point.z) * (float) (180.0/M_PI);
+ ao_sample_orient = acosf(rotz) * (float) (180.0/M_PI);
}
#endif
ao_sample_pitch = 0;
ao_sample_yaw = 0;
ao_sample_roll = 0;
- ao_orient = 0;
+ ao_sample_orient = 0;
#endif
ao_sample_data = ao_data_head;
ao_preflight = TRUE;