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refactor(LSM303DLHC): Converted functions to static functions

This commit is contained in:
Devoalda 2023-10-25 21:11:35 +08:00
parent e0c85ce2ce
commit 0f0b0a9886
2 changed files with 25 additions and 14 deletions
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3
frtos/config/magnetometer_config.h
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@ -7,6 +7,9 @@
#define DIRECTION_READ_DELAY ( 100 ) #define DIRECTION_READ_DELAY ( 100 )
#define ALPHA ( 0.98f ) // Complementary
// Filter Constant
/** /**
* @brief The orientation of the car * @brief The orientation of the car
*/ */

34
frtos/magnetometer/magnetometer_direction.h
View File

@ -10,7 +10,9 @@
* The roll, pitch and yaw are combined to calculate the direction * The roll, pitch and yaw are combined to calculate the direction
* of the car * of the car
* *
* The direction of the car is calculated using the complementary filter * The direction of the car is calculated using the complementary
* filter
*
* The complementary filter is used to combine the accelerometer * The complementary filter is used to combine the accelerometer
* and magnetometer data to calculate the direction of the car * and magnetometer data to calculate the direction of the car
* *
@ -26,7 +28,8 @@
* @param acceleration Accelerometer Data * @param acceleration Accelerometer Data
* @return * @return
*/ */
float calculate_roll(int16_t acceleration[3]) { static inline float
calculate_roll(int16_t acceleration[3]) {
return atan2(acceleration[1], acceleration[2]) * (180.0 / M_PI); return atan2(acceleration[1], acceleration[2]) * (180.0 / M_PI);
} }
@ -35,7 +38,8 @@ float calculate_roll(int16_t acceleration[3]) {
* @param acceleration Accelerometer Data * @param acceleration Accelerometer Data
* @return * @return
*/ */
float calculate_pitch(int16_t acceleration[3]) { static inline float
calculate_pitch(int16_t acceleration[3]) {
return atan2(- acceleration[0], sqrt(acceleration[1] * acceleration[1] + return atan2(- acceleration[0], sqrt(acceleration[1] * acceleration[1] +
acceleration[2] * acceleration[2])) * acceleration[2] * acceleration[2])) *
(180.0 / M_PI); (180.0 / M_PI);
@ -46,19 +50,20 @@ float calculate_pitch(int16_t acceleration[3]) {
* @param magnetometer Magnetometer Data * @param magnetometer Magnetometer Data
* @return * @return
*/ */
float calculate_yaw_magnetometer(int16_t magnetometer[3]) { static inline float
calculate_yaw_magnetometer(int16_t magnetometer[3]) {
return atan2(magnetometer[1], magnetometer[0]) * (180.0 / M_PI); return atan2(magnetometer[1], magnetometer[0]) * (180.0 / M_PI);
} }
/** /**
* @brief Complementary Filter for Yaw * @brief Complementary Filter for Yaw
* @param alpha Complementary Filter Constant
* @param yaw_acc Yaw calculated from Accelerometer Data * @param yaw_acc Yaw calculated from Accelerometer Data
* @param yaw_mag Yaw calculated from Magnetometer Data * @param yaw_mag Yaw calculated from Magnetometer Data
* @return yaw Yaw calculated from Complementary Filter * @return yaw Yaw calculated from Complementary Filter
*/ */
float calculate_yaw_complementary(float alpha, float yaw_acc, float yaw_mag) { static inline float
return alpha * yaw_acc + (1 - alpha) * yaw_mag; calculate_yaw_complementary(float yaw_acc, float yaw_mag) {
return ALPHA * yaw_acc + (1 - ALPHA) * yaw_mag;
} }
/** /**
@ -66,7 +71,8 @@ float calculate_yaw_complementary(float alpha, float yaw_acc, float yaw_mag) {
* @param yaw Yaw calculated from Complementary Filter * @param yaw Yaw calculated from Complementary Filter
* @return yaw Yaw adjusted to be between 0 and 360 degrees * @return yaw Yaw adjusted to be between 0 and 360 degrees
*/ */
float adjust_yaw(float yaw) { static inline float
adjust_yaw(float yaw) {
return (yaw < 0) ? yaw + 360.0f : yaw; return (yaw < 0) ? yaw + 360.0f : yaw;
} }
@ -77,7 +83,8 @@ float adjust_yaw(float yaw) {
* @param yaw Yaw calculated from Complementary Filter * @param yaw Yaw calculated from Complementary Filter
* @return Compass Direction * @return Compass Direction
*/ */
compass_direction_t calculate_compass_direction(float yaw) { static inline compass_direction_t
calculate_compass_direction(float yaw) {
int orientation = (int) ((yaw + 22.5) / 45.0) % 8; // 8 compass directions int orientation = (int) ((yaw + 22.5) / 45.0) % 8; // 8 compass directions
switch (orientation) switch (orientation)
{ {
@ -109,7 +116,8 @@ compass_direction_t calculate_compass_direction(float yaw) {
* @param yaw Yaw calculated from Complementary Filter * @param yaw Yaw calculated from Complementary Filter
* @param compass_direction Compass Direction * @param compass_direction Compass Direction
*/ */
void update_orientation_data(float roll, float pitch, float yaw, static inline void
update_orientation_data(float roll, float pitch, float yaw,
compass_direction_t compass_direction) { compass_direction_t compass_direction) {
g_direction.roll = roll; g_direction.roll = roll;
g_direction.pitch = pitch; g_direction.pitch = pitch;
@ -124,14 +132,14 @@ void update_orientation_data(float roll, float pitch, float yaw,
* @param acceleration Accelerometer Data * @param acceleration Accelerometer Data
* @param magnetometer Magnetometer Data * @param magnetometer Magnetometer Data
*/ */
static void read_direction(int16_t acceleration[3], int16_t magnetometer[3]) { static void
read_direction(int16_t acceleration[3], int16_t magnetometer[3]) {
float roll = calculate_roll(acceleration); float roll = calculate_roll(acceleration);
float pitch = calculate_pitch(acceleration); float pitch = calculate_pitch(acceleration);
float yaw_mag = calculate_yaw_magnetometer(magnetometer); float yaw_mag = calculate_yaw_magnetometer(magnetometer);
float alpha = 0.98;
float yaw_acc = atan2(acceleration[1], acceleration[0]) * (180.0 / M_PI); float yaw_acc = atan2(acceleration[1], acceleration[0]) * (180.0 / M_PI);
float yaw = calculate_yaw_complementary(alpha, yaw_acc, yaw_mag); float yaw = calculate_yaw_complementary(yaw_acc, yaw_mag);
yaw = adjust_yaw(yaw); yaw = adjust_yaw(yaw);