From bdd6244d8b4a55c9aa4fb79b0cb1a0727afbc2ac Mon Sep 17 00:00:00 2001 From: Keith Packard Date: Tue, 12 Nov 2013 14:01:55 +0900 Subject: [PATCH] altos: Add orientation tracking to ao_flight_test Shows calculated offset from vertical in ao_flight_test output Signed-off-by: Keith Packard --- src/core/ao_data.h | 12 +++++ src/core/ao_quaternion.h | 9 ++++ src/test/ao_flight_test.c | 111 ++++++++++++++++++++++++++++++++++++-- 3 files changed, 127 insertions(+), 5 deletions(-) diff --git a/src/core/ao_data.h b/src/core/ao_data.h index 5a232885..e1d8a139 100644 --- a/src/core/ao_data.h +++ b/src/core/ao_data.h @@ -319,4 +319,16 @@ typedef int16_t angle_t; /* in degrees */ #endif +#if !HAS_MAG && HAS_HMC5883 + +#define HAS_MAG 1 + +typedef int16_t ao_mag_t; /* in raw sample units */ + +#define ao_data_mag_along(packet) ((packet)->hmc5883.x) +#define ao_data_mag_across(packet) ((packet)->hmc5883.y) +#define ao_data_mag_through(packet) ((packet)->hmc5883.z) + +#endif + #endif /* _AO_DATA_H_ */ diff --git a/src/core/ao_quaternion.h b/src/core/ao_quaternion.h index 6c885500..044f1607 100644 --- a/src/core/ao_quaternion.h +++ b/src/core/ao_quaternion.h @@ -109,6 +109,15 @@ static inline void ao_quaternion_normalize(struct ao_quaternion *r, *r = *a; } +static inline float ao_quaternion_dot(const struct ao_quaternion *a, + const struct ao_quaternion *b) +{ +#define T(_a) (((a)->_a) * ((b)->_a)) + return T(r) + T(x) + T(y) + T(z); +#undef T +} + + static inline void ao_quaternion_rotate(struct ao_quaternion *r, const struct ao_quaternion *a, const struct ao_quaternion *b) diff --git a/src/test/ao_flight_test.c b/src/test/ao_flight_test.c index 952a811a..452f5b75 100644 --- a/src/test/ao_flight_test.c +++ b/src/test/ao_flight_test.c @@ -48,6 +48,7 @@ int ao_gps_new; #define HAS_MS5607 1 #define HAS_MPU6000 1 #define HAS_MMA655X 1 +#define HAS_HMC5883 1 struct ao_adc { int16_t sense[AO_ADC_NUM_SENSE]; @@ -349,6 +350,23 @@ ao_test_exit(void) exit(0); } +#ifdef TELEMEGA +struct ao_azel { + int az; + int el; +}; + +static void +azel (struct ao_azel *r, struct ao_quaternion *q) +{ + double v; + + r->az = floor (atan2(q->y, q->x) * 180/M_PI + 0.5); + v = sqrt (q->x*q->x + q->y*q->y); + r->el = floor (atan2(q->z, v) * 180/M_PI + 0.5); +} +#endif + void ao_insert(void) { @@ -402,10 +420,86 @@ ao_insert(void) } if (!ao_summary) { +#if TELEMEGA + static struct ao_quaternion ao_ground_mag; + static int ao_ground_mag_set; + + if (!ao_ground_mag_set) { + ao_quaternion_init_vector (&ao_ground_mag, + ao_data_mag_across(&ao_data_static), + ao_data_mag_through(&ao_data_static), + ao_data_mag_along(&ao_data_static)); + ao_quaternion_normalize(&ao_ground_mag, &ao_ground_mag); + ao_quaternion_rotate(&ao_ground_mag, &ao_ground_mag, &ao_rotation); + ao_ground_mag_set = 1; + } + + struct ao_quaternion ao_mag, ao_mag_rot; + + ao_quaternion_init_vector(&ao_mag, + ao_data_mag_across(&ao_data_static), + ao_data_mag_through(&ao_data_static), + ao_data_mag_along(&ao_data_static)); + + ao_quaternion_normalize(&ao_mag, &ao_mag); + ao_quaternion_rotate(&ao_mag_rot, &ao_mag, &ao_rotation); + + float ao_dot; + int ao_mag_angle; + + ao_dot = ao_quaternion_dot(&ao_mag_rot, &ao_ground_mag); + + struct ao_azel ground_azel, mag_azel, rot_azel; + + azel(&ground_azel, &ao_ground_mag); + azel(&mag_azel, &ao_mag); + azel(&rot_azel, &ao_mag_rot); + + ao_mag_angle = floor (acos(ao_dot) * 180 / M_PI + 0.5); + + static struct ao_quaternion ao_x = { .r = 0, .x = 1, .y = 0, .z = 0 }; + struct ao_quaternion ao_out; + + ao_quaternion_rotate(&ao_out, &ao_x, &ao_rotation); + + int out = floor (atan2(ao_out.y, ao_out.x) * 180 / M_PI); + + printf ("%7.2f state %-8.8s height %8.4f tilt %4d rot %4d mag_tilt %4d mag_rot %4d\n", + time, + ao_state_names[ao_flight_state], + ao_k_height / 65536.0, + ao_sample_orient, out, + mag_azel.el, + mag_azel.az); + + +#if 0 + printf ("\t\tstate %-8.8s ground az: %4d el %4d mag az %4d el %4d rot az %4d el %4d el_diff %4d az_diff %4d angle %4d tilt %4d ground %8.5f %8.5f %8.5f cur %8.5f %8.5f %8.5f rot %8.5f %8.5f %8.5f\n", + ao_state_names[ao_flight_state], + ground_azel.az, ground_azel.el, + mag_azel.az, mag_azel.el, + rot_azel.az, rot_azel.el, + ground_azel.el - rot_azel.el, + ground_azel.az - rot_azel.az, + ao_mag_angle, + ao_sample_orient, + ao_ground_mag.x, + ao_ground_mag.y, + ao_ground_mag.z, + ao_mag.x, + ao_mag.y, + ao_mag.z, + ao_mag_rot.x, + ao_mag_rot.y, + ao_mag_rot.z); +#endif +#endif + +#if 0 printf("%7.2f height %8.2f accel %8.3f " #if TELEMEGA "angle %5d " -/* "accel_x %8.3f accel_y %8.3f accel_z %8.3f gyro_x %8.3f gyro_y %8.3f gyro_z %8.3f " */ + "accel_x %8.3f accel_y %8.3f accel_z %8.3f gyro_x %8.3f gyro_y %8.3f gyro_z %8.3f mag_x %8d mag_y %8d, mag_z %8d mag_angle %4d " #endif "state %-8.8s k_height %8.2f k_speed %8.3f k_accel %8.3f avg_height %5d drogue %4d main %4d error %5d\n", time, @@ -413,14 +507,17 @@ ao_insert(void) accel, #if TELEMEGA ao_sample_orient, -/* + ao_mpu6000_accel(ao_data_static.mpu6000.accel_x), ao_mpu6000_accel(ao_data_static.mpu6000.accel_y), ao_mpu6000_accel(ao_data_static.mpu6000.accel_z), ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_x - ao_ground_mpu6000.gyro_x), ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_y - ao_ground_mpu6000.gyro_y), ao_mpu6000_gyro(ao_data_static.mpu6000.gyro_z - ao_ground_mpu6000.gyro_z), -*/ + ao_data_static.hmc5883.x, + ao_data_static.hmc5883.y, + ao_data_static.hmc5883.z, + ao_mag_angle, #endif ao_state_names[ao_flight_state], ao_k_height / 65536.0, @@ -430,6 +527,7 @@ ao_insert(void) drogue_height, main_height, ao_error_h_sq_avg); +#endif // if (ao_flight_state == ao_flight_landed) // ao_test_exit(); @@ -659,11 +757,14 @@ ao_sleep(void *wchan) ao_data_static.ms5607_raw.temp = int32(bytes, 4); ao_ms5607_convert(&ao_data_static.ms5607_raw, &value); ao_data_static.mpu6000.accel_x = int16(bytes, 8); - ao_data_static.mpu6000.accel_y = -int16(bytes, 10); + ao_data_static.mpu6000.accel_y = int16(bytes, 10); ao_data_static.mpu6000.accel_z = int16(bytes, 12); ao_data_static.mpu6000.gyro_x = int16(bytes, 14); - ao_data_static.mpu6000.gyro_y = -int16(bytes, 16); + ao_data_static.mpu6000.gyro_y = int16(bytes, 16); ao_data_static.mpu6000.gyro_z = int16(bytes, 18); + ao_data_static.hmc5883.x = int16(bytes, 20); + ao_data_static.hmc5883.y = int16(bytes, 22); + ao_data_static.hmc5883.z = int16(bytes, 24); #if HAS_MMA655X ao_data_static.mma655x = int16(bytes, 26); #endif -- 2.30.2