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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-05-22 15:17:35 +08:00
To use freeIMU processing visualization tool, I have implemented float number transmission over uart (default /dev/ttyS2, 115200)
But this not tested yet. I should.
This commit is contained in:
@@ -47,6 +47,10 @@ static int attitude_estimator_so3_comp_task; /**< Handle of deamon task / thr
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static float q0 = 1.0f, q1 = 0.0f, q2 = 0.0f, q3 = 0.0f; // quaternion of sensor frame relative to auxiliary frame
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static float integralFBx = 0.0f, integralFBy = 0.0f, integralFBz = 0.0f; // integral error terms scaled by Ki
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//! Serial packet related
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static int uart;
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static int baudrate;
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/**
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* Mainloop of attitude_estimator_so3_comp.
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*/
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@@ -63,7 +67,9 @@ usage(const char *reason)
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if (reason)
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fprintf(stderr, "%s\n", reason);
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fprintf(stderr, "usage: attitude_estimator_so3_comp {start|stop|status} [-p <additional params>]\n\n");
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fprintf(stderr, "usage: attitude_estimator_so3_comp {start|stop|status} [-d <devicename>] [-b <baud rate>]\n"
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"-d and -b options are for separate visualization with raw data (quaternion packet) transfer\n"
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"ex) attitude_estimator_so3_comp start -d /dev/ttyS1 -b 115200\n");
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exit(1);
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}
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@@ -80,6 +86,8 @@ int attitude_estimator_so3_comp_main(int argc, char *argv[])
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if (argc < 1)
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usage("missing command");
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if (!strcmp(argv[1], "start")) {
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if (thread_running) {
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@@ -94,12 +102,18 @@ int attitude_estimator_so3_comp_main(int argc, char *argv[])
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SCHED_PRIORITY_MAX - 5,
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12400,
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attitude_estimator_so3_comp_thread_main,
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(argv) ? (const char **)&argv[2] : (const char **)NULL);
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(const char **)argv);
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exit(0);
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}
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if (!strcmp(argv[1], "stop")) {
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thread_should_exit = true;
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while(thread_running){
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usleep(200000);
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printf(".");
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}
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printf("terminated.");
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exit(0);
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}
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@@ -121,76 +135,18 @@ int attitude_estimator_so3_comp_main(int argc, char *argv[])
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//---------------------------------------------------------------------------------------------------
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// Fast inverse square-root
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// See: http://en.wikipedia.org/wiki/Fast_inverse_square_root
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float invSqrt(float x) {
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float halfx = 0.5f * x;
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float y = x;
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long i = *(long*)&y;
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i = 0x5f3759df - (i>>1);
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y = *(float*)&i;
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y = y * (1.5f - (halfx * y * y));
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return y;
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}
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float invSqrt(float number) {
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volatile long i;
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volatile float x, y;
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volatile const float f = 1.5F;
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void MahonyAHRSupdateIMU(float gx, float gy, float gz, float ax, float ay, float az, float twoKp, float twoKi, float dt) {
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float recipNorm;
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float halfvx, halfvy, halfvz;
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float halfex, halfey, halfez;
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// Compute feedback only if accelerometer measurement valid (avoids NaN in accelerometer normalisation)
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if(!((ax == 0.0f) && (ay == 0.0f) && (az == 0.0f))) {
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// Normalise accelerometer measurement
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recipNorm = invSqrt(ax * ax + ay * ay + az * az);
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ax *= recipNorm;
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ay *= recipNorm;
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az *= recipNorm;
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// Estimated direction of gravity and vector perpendicular to magnetic flux
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halfvx = q1 * q3 - q0 * q2;
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halfvy = q0 * q1 + q2 * q3;
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halfvz = q0 * q0 - 0.5f + q3 * q3;
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// Error is sum of cross product between estimated and measured direction of gravity
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halfex = (ay * halfvz - az * halfvy);
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halfey = (az * halfvx - ax * halfvz);
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halfez = (ax * halfvy - ay * halfvx);
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// Compute and apply integral feedback if enabled
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if(twoKi > 0.0f) {
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integralFBx += twoKi * halfex * dt; // integral error scaled by Ki
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integralFBy += twoKi * halfey * dt;
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integralFBz += twoKi * halfez * dt;
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gx += integralFBx; // apply integral feedback
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gy += integralFBy;
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gz += integralFBz;
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}
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else {
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integralFBx = 0.0f; // prevent integral windup
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integralFBy = 0.0f;
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integralFBz = 0.0f;
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}
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// Apply proportional feedback
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gx += twoKp * halfex;
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gy += twoKp * halfey;
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gz += twoKp * halfez;
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}
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// Integrate rate of change of quaternion
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gx *= (0.5f * dt); // pre-multiply common factors
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gy *= (0.5f * dt);
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gz *= (0.5f * dt);
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q0 +=(-q1 * gx - q2 * gy - q3 * gz);
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q1 += (q0 * gx + q2 * gz - q3 * gy);
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q2 += (q0 * gy - q1 * gz + q3 * gx);
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q3 += (q0 * gz + q1 * gy - q2 * gx);
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// Normalise quaternion
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recipNorm = invSqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3);
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q0 *= recipNorm;
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q1 *= recipNorm;
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q2 *= recipNorm;
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q3 *= recipNorm;
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x = number * 0.5F;
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y = number;
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i = * (( long * ) &y);
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i = 0x5f375a86 - ( i >> 1 );
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y = * (( float * ) &i);
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y = y * ( f - ( x * y * y ) );
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return y;
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}
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void MahonyAHRSupdate(float gx, float gy, float gz, float ax, float ay, float az, float mx, float my, float mz, float twoKp, float twoKi, float dt) {
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@@ -202,7 +158,7 @@ void MahonyAHRSupdate(float gx, float gy, float gz, float ax, float ay, float az
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// Use IMU algorithm if magnetometer measurement invalid (avoids NaN in magnetometer normalisation)
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if((mx == 0.0f) && (my == 0.0f) && (mz == 0.0f)) {
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MahonyAHRSupdateIMU(gx, gy, gz, ax, ay, az, twoKp, twoKi, dt);
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//MahonyAHRSupdateIMU(gx, gy, gz, ax, ay, az, twoKp, twoKi, dt);
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return;
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}
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@@ -290,6 +246,117 @@ void MahonyAHRSupdate(float gx, float gy, float gz, float ax, float ay, float az
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q3 *= recipNorm;
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}
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void send_uart_byte(char c)
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{
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write(uart,&c,1);
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}
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void send_uart_bytes(uint8_t *data, int length)
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{
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write(uart,data,(size_t)(sizeof(uint8_t)*length));
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}
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void send_uart_float(float f) {
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uint8_t * b = (uint8_t *) &f;
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//! Assume float is 4-bytes
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for(int i=0; i<4; i++) {
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uint8_t b1 = (b[i] >> 4) & 0x0f;
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uint8_t b2 = (b[i] & 0x0f);
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uint8_t c1 = (b1 < 10) ? ('0' + b1) : 'A' + b1 - 10;
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uint8_t c2 = (b2 < 10) ? ('0' + b2) : 'A' + b2 - 10;
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send_uart_bytes(&c1,1);
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send_uart_bytes(&c2,1);
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}
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}
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void send_uart_float_arr(float *arr, int length)
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{
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for(int i=0;i<length;++i)
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{
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send_uart_float(arr[i]);
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send_uart_byte(',');
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}
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}
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int open_uart(int baud, const char *uart_name, struct termios *uart_config_original, bool *is_usb)
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{
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int speed;
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switch (baud) {
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case 0: speed = B0; break;
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case 50: speed = B50; break;
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case 75: speed = B75; break;
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case 110: speed = B110; break;
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case 134: speed = B134; break;
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case 150: speed = B150; break;
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case 200: speed = B200; break;
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case 300: speed = B300; break;
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case 600: speed = B600; break;
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case 1200: speed = B1200; break;
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case 1800: speed = B1800; break;
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case 2400: speed = B2400; break;
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case 4800: speed = B4800; break;
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case 9600: speed = B9600; break;
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case 19200: speed = B19200; break;
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case 38400: speed = B38400; break;
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case 57600: speed = B57600; break;
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case 115200: speed = B115200; break;
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case 230400: speed = B230400; break;
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case 460800: speed = B460800; break;
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case 921600: speed = B921600; break;
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default:
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fprintf(stderr, "ERROR: Unsupported baudrate: %d\n\tsupported examples:\n\n\t9600\n19200\n38400\n57600\n115200\n230400\n460800\n921600\n\n", baud);
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return -EINVAL;
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}
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printf("[mavlink] UART is %s, baudrate is %d\n", uart_name, baud);
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uart = open(uart_name, O_RDWR | O_NOCTTY);
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/* Try to set baud rate */
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struct termios uart_config;
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int termios_state;
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*is_usb = false;
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/* make some wild guesses including that USB serial is indicated by either /dev/ttyACM0 or /dev/console */
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if (strcmp(uart_name, "/dev/ttyACM0") != OK && strcmp(uart_name, "/dev/console") != OK) {
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/* Back up the original uart configuration to restore it after exit */
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if ((termios_state = tcgetattr(uart, uart_config_original)) < 0) {
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fprintf(stderr, "ERROR getting baudrate / termios config for %s: %d\n", uart_name, termios_state);
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close(uart);
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return -1;
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}
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/* Fill the struct for the new configuration */
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tcgetattr(uart, &uart_config);
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/* Clear ONLCR flag (which appends a CR for every LF) */
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uart_config.c_oflag &= ~ONLCR;
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/* Set baud rate */
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if (cfsetispeed(&uart_config, speed) < 0 || cfsetospeed(&uart_config, speed) < 0) {
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fprintf(stderr, "ERROR setting baudrate / termios config for %s: %d (cfsetispeed, cfsetospeed)\n", uart_name, termios_state);
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close(uart);
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return -1;
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}
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if ((termios_state = tcsetattr(uart, TCSANOW, &uart_config)) < 0) {
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fprintf(stderr, "ERROR setting baudrate / termios config for %s (tcsetattr)\n", uart_name);
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close(uart);
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return -1;
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}
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} else {
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*is_usb = true;
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}
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return uart;
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}
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/*
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* [Rot_matrix,x_aposteriori,P_aposteriori] = attitudeKalmanfilter(dt,z_k,x_aposteriori_k,P_aposteriori_k,knownConst)
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*/
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@@ -307,6 +374,15 @@ int attitude_estimator_so3_comp_thread_main(int argc, char *argv[])
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const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
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//! Serial debug related
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int ch;
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struct termios uart_config_original;
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bool usb_uart;
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bool debug_mode = false;
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char *device_name = "/dev/ttyS2";
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baudrate = 115200;
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//! Time constant
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float dt = 0.005f;
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/* output euler angles */
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@@ -321,6 +397,34 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
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float gyro[3] = {0.0f, 0.0f, 0.0f};
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float mag[3] = {0.0f, 0.0f, 0.0f};
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/* work around some stupidity in task_create's argv handling */
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argc -= 2;
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argv += 2;
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//! -d <device_name>, default : /dev/ttyS2
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//! -b <baud_rate>, default : 115200
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while ((ch = getopt(argc,argv,"d:b:")) != EOF){
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switch(ch){
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case 'b':
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baudrate = strtoul(optarg, NULL, 10);
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if(baudrate == 0)
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printf("invalid baud rate '%s'",optarg);
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break;
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case 'd':
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device_name = optarg;
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debug_mode = true;
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break;
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default:
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usage("invalid argument");
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}
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}
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if(debug_mode){
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uart = open_uart(baudrate, device_name, &uart_config_original, &usb_uart);
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if (uart < 0)
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printf("could not open %s", device_name);
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}
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// print text
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printf("Nonlinear SO3 Attitude Estimator initialized..\n\n");
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fflush(stdout);
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@@ -554,9 +658,9 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
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}
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*/
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euler[0] = atan2f(2*(q0*q1+q2*q3),1-2*(q1*q1+q2*q2));
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euler[1] = asinf(2*(q0*q2-q3*q1));
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euler[2] = atan2f(2*(q0*q3+q1*q2),1-2*(q2*q2+q3*q3));
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euler[2] = atan2f(2*(q1*q2-q0*q3),2*(q0*q0+q1*q1)-1);
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euler[1]= -asinf(2*(q1*q3+q0*q2));
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euler[0] = atan2f(2*(q2*q3-q0*q1),2*(q0*q0+q3*q3)-1);
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/* swap values for next iteration, check for fatal inputs */
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@@ -607,7 +711,18 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
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}
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perf_end(so3_comp_loop_perf);
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}
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if(debug_mode)
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{
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float quat[4];
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quat[0] = q0;
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quat[1] = q1;
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quat[2] = q2;
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quat[3] = q3;
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send_uart_float_arr(quat,4);
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send_uart_byte('\n');
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}
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}// else
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}
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}
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@@ -616,5 +731,9 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
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thread_running = false;
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/* Reset the UART flags to original state */
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if (!usb_uart)
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tcsetattr(uart, TCSANOW, &uart_config_original);
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return 0;
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}
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Reference in New Issue
Block a user