mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-15 02:03:33 +08:00
Merge branch 'master' of https://github.com/PX4/Firmware
This commit is contained in:
@@ -60,6 +60,7 @@
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#include <systemlib/param/param.h>
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#include <systemlib/pid/pid.h>
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#include <systemlib/geo/geo.h>
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#include <uORB/topics/debug_key_value.h>
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static bool thread_should_exit = false; /**< Deamon exit flag */
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static bool thread_running = false; /**< Deamon status flag */
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@@ -158,14 +159,14 @@ static int pos_parameters_update(const struct fw_pos_control_param_handles *h, s
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*/
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int fixedwing_control_thread_main(int argc, char *argv[])
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{
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// /* read arguments */
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// bool verbose = false;
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/* read arguments */
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bool verbose = false;
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// for (int i = 1; i < argc; i++) {
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// if (strcmp(argv[i], "-v") == 0 || strcmp(argv[i], "--verbose") == 0) {
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// verbose = true;
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// }
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// }
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for (int i = 1; i < argc; i++) {
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if (strcmp(argv[i], "-v") == 0 || strcmp(argv[i], "--verbose") == 0) {
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verbose = true;
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}
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}
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/* welcome user */
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printf("[fixedwing control] started\n");
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@@ -229,6 +230,11 @@ int fixedwing_control_thread_main(int argc, char *argv[])
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pid_init(&heading_controller, ppos.heading_p, 0.0f, 0.0f, 0.0f,
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PID_MODE_DERIVATIV_SET);
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// XXX remove in production
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/* advertise debug value */
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struct debug_key_value_s dbg = { .key = "", .value = 0.0f };
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orb_advert_t pub_dbg = orb_advertise(ORB_ID(debug_key_value), &dbg);
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while(!thread_should_exit) {
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struct pollfd fds[1] = {
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@@ -268,7 +274,11 @@ int fixedwing_control_thread_main(int argc, char *argv[])
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/* get a local copy of attitude */
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orb_copy(ORB_ID(vehicle_attitude), att_sub, &att);
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/* get a local copy of attitude setpoint */
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orb_copy(ORB_ID(vehicle_attitude_setpoint), att_setpoint_sub, &att_sp);
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//orb_copy(ORB_ID(vehicle_attitude_setpoint), att_setpoint_sub, &att_sp);
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// XXX update to switch between external attitude reference and the
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// attitude calculated here
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char name[10];
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if (pos_updated) {
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@@ -288,7 +298,14 @@ int fixedwing_control_thread_main(int argc, char *argv[])
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global_setpoint.lat / (double)1e7d, global_setpoint.lon / (double)1e7d);
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/* shift error to prevent wrapping issues */
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float bearing_error = att.yaw - target_bearing;
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float bearing_error = target_bearing - att.yaw;
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if (loopcounter % 2 == 0) {
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sprintf(name, "hdng err1");
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memcpy(dbg.key, name, sizeof(name));
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dbg.value = bearing_error;
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orb_publish(ORB_ID(debug_key_value), pub_dbg, &dbg);
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}
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if (bearing_error < M_PI_F) {
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bearing_error += 2.0f * M_PI_F;
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@@ -298,6 +315,13 @@ int fixedwing_control_thread_main(int argc, char *argv[])
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bearing_error -= 2.0f * M_PI_F;
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}
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if (loopcounter % 2 != 0) {
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sprintf(name, "hdng err2");
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memcpy(dbg.key, name, sizeof(name));
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dbg.value = bearing_error;
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orb_publish(ORB_ID(debug_key_value), pub_dbg, &dbg);
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}
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/* calculate roll setpoint, do this artificially around zero */
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att_sp.roll_body = pid_calculate(&heading_controller, bearing_error,
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0.0f, att.yawspeed, deltaT);
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@@ -313,7 +337,6 @@ int fixedwing_control_thread_main(int argc, char *argv[])
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heading_controller.saturated = 1;
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}
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att_sp.roll_body = att_sp.roll_body;
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att_sp.pitch_body = 0.0f;
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att_sp.yaw_body = 0.0f;
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@@ -331,7 +354,13 @@ int fixedwing_control_thread_main(int argc, char *argv[])
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const float deltaTpos = (hrt_absolute_time() - last_run_pos) / 1000000.0f;
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last_run_pos = hrt_absolute_time();
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actuators.control[0] = pid_calculate(&roll_pos_controller, att_sp.roll_body,
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if (verbose && (loopcounter % 20 == 0)) {
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printf("[fixedwing control] roll sp: %8.4f, \n", att_sp.roll_body);
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}
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// actuators.control[0] = pid_calculate(&roll_pos_controller, att_sp.roll_body,
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// att.roll, att.rollspeed, deltaTpos);
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actuators.control[0] = pid_calculate(&roll_pos_controller, att_sp.roll_body,
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att.roll, att.rollspeed, deltaTpos);
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actuators.control[1] = 0;
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actuators.control[2] = 0;
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@@ -1416,15 +1416,15 @@ void handleMessage(mavlink_message_t *msg)
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memset(&rc_hil, 0, sizeof(rc_hil));
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static orb_advert_t rc_pub = 0;
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rc_hil.chan[0].raw = 1510 + man.x / 2;
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rc_hil.chan[1].raw = 1520 + man.y / 2;
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rc_hil.chan[2].raw = 1590 + man.r / 2;
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rc_hil.chan[3].raw = 1420 + man.z / 2;
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rc_hil.chan[0].raw = 1500 + man.x / 2;
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rc_hil.chan[1].raw = 1500 + man.y / 2;
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rc_hil.chan[2].raw = 1500 + man.r / 2;
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rc_hil.chan[3].raw = 1500 + man.z / 2;
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rc_hil.chan[0].scaled = man.x;
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rc_hil.chan[1].scaled = man.y;
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rc_hil.chan[2].scaled = man.r;
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rc_hil.chan[3].scaled = man.z;
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rc_hil.chan[0].scaled = man.x / 1000.0f;
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rc_hil.chan[1].scaled = man.y / 1000.0f;
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rc_hil.chan[2].scaled = man.r / 1000.0f;
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rc_hil.chan[3].scaled = man.z / 1000.0f;
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struct manual_control_setpoint_s mc;
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static orb_advert_t mc_pub = 0;
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@@ -1432,7 +1432,7 @@ void handleMessage(mavlink_message_t *msg)
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mc.roll = man.x / 1000.0f;
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mc.pitch = man.y / 1000.0f;
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mc.yaw = man.r / 1000.0f;
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mc.roll = man.z / 1000.0f;
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mc.throttle = man.z / 1000.0f;
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/* fake RC channels with manual control input from simulator */
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+43
-21
@@ -66,7 +66,6 @@
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#include <uORB/topics/actuator_controls.h>
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#include <uORB/topics/actuator_outputs.h>
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class FMUServo : public device::CDev
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{
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public:
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@@ -75,7 +74,7 @@ public:
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MODE_4PWM,
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MODE_NONE
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};
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FMUServo(Mode mode);
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FMUServo(Mode mode, int update_rate);
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~FMUServo();
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virtual int ioctl(struct file *filp, int cmd, unsigned long arg);
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@@ -86,6 +85,7 @@ private:
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static const unsigned _max_actuators = 4;
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Mode _mode;
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int _update_rate;
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int _task;
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int _t_actuators;
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int _t_armed;
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@@ -115,9 +115,10 @@ FMUServo *g_servo;
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} // namespace
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FMUServo::FMUServo(Mode mode) :
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FMUServo::FMUServo(Mode mode, int update_rate) :
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CDev("fmuservo", PWM_OUTPUT_DEVICE_PATH),
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_mode(mode),
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_update_rate(update_rate),
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_task(-1),
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_t_actuators(-1),
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_t_armed(-1),
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@@ -199,6 +200,8 @@ FMUServo::task_main()
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/* multi-port as 4 PWM outs */
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/* XXX magic numbers */
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up_pwm_servo_init(0xf);
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/* set the update rate for 4 PWM mode only for now */
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up_pwm_servo_set_rate(_update_rate);
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break;
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case MODE_NONE:
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@@ -208,7 +211,9 @@ FMUServo::task_main()
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/* subscribe to objects that we are interested in watching */
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_t_actuators = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS);
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orb_set_interval(_t_actuators, 20); /* 50Hz update rate */
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/* convert the update rate in hz to milliseconds, rounding down if necessary */
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int update_rate_in_ms = int(1000 / _update_rate);
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orb_set_interval(_t_actuators, update_rate_in_ms);
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_t_armed = orb_subscribe(ORB_ID(actuator_armed));
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orb_set_interval(_t_armed, 200); /* 5Hz update rate */
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@@ -444,7 +449,7 @@ enum PortMode {
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PortMode g_port_mode;
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int
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fmu_new_mode(PortMode new_mode)
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fmu_new_mode(PortMode new_mode, int update_rate)
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{
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int fd;
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int ret = OK;
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@@ -511,7 +516,7 @@ fmu_new_mode(PortMode new_mode)
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/* create new PWM driver if required */
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if (servo_mode != FMUServo::MODE_NONE) {
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g_servo = new FMUServo(servo_mode);
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g_servo = new FMUServo(servo_mode, update_rate);
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if (g_servo == nullptr) {
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ret = -ENOMEM;
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@@ -585,6 +590,7 @@ int
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fmu_main(int argc, char *argv[])
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{
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PortMode new_mode = PORT_MODE_UNSET;
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int pwm_update_rate_in_hz = 50;
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if (!strcmp(argv[1], "test"))
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test();
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@@ -597,24 +603,40 @@ fmu_main(int argc, char *argv[])
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*
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* XXX use getopt?
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*/
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if (!strcmp(argv[1], "mode_gpio")) {
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new_mode = PORT_FULL_GPIO;
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for (int i = 1; i < argc; i++) { /* argv[0] is "fmu" */
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if (!strcmp(argv[i], "mode_gpio")) {
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new_mode = PORT_FULL_GPIO;
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} else if (!strcmp(argv[1], "mode_serial")) {
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new_mode = PORT_FULL_SERIAL;
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} else if (!strcmp(argv[i], "mode_serial")) {
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new_mode = PORT_FULL_SERIAL;
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} else if (!strcmp(argv[1], "mode_pwm")) {
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new_mode = PORT_FULL_PWM;
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} else if (!strcmp(argv[i], "mode_pwm")) {
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new_mode = PORT_FULL_PWM;
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} else if (!strcmp(argv[1], "mode_gpio_serial")) {
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new_mode = PORT_GPIO_AND_SERIAL;
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} else if (!strcmp(argv[i], "mode_gpio_serial")) {
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new_mode = PORT_GPIO_AND_SERIAL;
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} else if (!strcmp(argv[1], "mode_pwm_serial")) {
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new_mode = PORT_PWM_AND_SERIAL;
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} else if (!strcmp(argv[i], "mode_pwm_serial")) {
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new_mode = PORT_PWM_AND_SERIAL;
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} else if (!strcmp(argv[1], "mode_pwm_gpio")) {
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new_mode = PORT_PWM_AND_GPIO;
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}
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} else if (!strcmp(argv[i], "mode_pwm_gpio")) {
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new_mode = PORT_PWM_AND_GPIO;
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}
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/* look for the optional pwm update rate for the supported modes */
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if (strcmp(argv[i], "-u") == 0 || strcmp(argv[i], "--update-rate") == 0) {
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if (new_mode == PORT_FULL_PWM || new_mode == PORT_PWM_AND_GPIO) {
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if (argc > i + 1) {
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pwm_update_rate_in_hz = atoi(argv[i + 1]);
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} else {
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fprintf(stderr, "missing argument for pwm update rate (-u)\n");
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return 1;
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}
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} else {
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fprintf(stderr, "pwm update rate currently only supported for mode_pwm, mode_pwm_gpio\n");
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}
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}
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}
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/* was a new mode set? */
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if (new_mode != PORT_MODE_UNSET) {
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@@ -624,12 +646,12 @@ fmu_main(int argc, char *argv[])
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return OK;
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/* switch modes */
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return fmu_new_mode(new_mode);
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return fmu_new_mode(new_mode, pwm_update_rate_in_hz);
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}
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/* test, etc. here */
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fprintf(stderr, "FMU: unrecognised command, try:\n");
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fprintf(stderr, " mode_gpio, mode_serial, mode_pwm, mode_gpio_serial, mode_pwm_serial, mode_pwm_gpio\n");
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fprintf(stderr, " mode_gpio, mode_serial, mode_pwm [-r pwm_update_rate_in_hz], mode_gpio_serial, mode_pwm_serial, mode_pwm_gpio\n");
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return -EINVAL;
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}
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@@ -79,9 +79,12 @@ __EXPORT float get_bearing_to_next_waypoint(double lat_now, double lon_now, doub
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/* conscious mix of double and float trig function to maximize speed and efficiency */
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float theta = atan2f(sin(d_lon) * cos(lat_next_rad) , cos(lat_now_rad) * sin(lat_next_rad) - sin(lat_now_rad) * cos(lat_next_rad) * cos(d_lon));
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// XXX wrapping check is incomplete
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if (theta < 0.0f) {
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theta = theta + 2.0f * M_PI_F;
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if (theta < M_PI_F) {
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theta += 2.0f * M_PI_F;
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}
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if (theta > M_PI_F) {
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theta -= 2.0f * M_PI_F;
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}
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return theta;
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@@ -179,7 +179,7 @@ __EXPORT float pid_calculate(PID_t *pid, float sp, float val, float val_dot, flo
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pid->error_previous = error;
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}
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float output = (error * pid->kp) + (i * pid->ki) + (d * pid->kd);
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float output = (pid->error_previous * pid->kp) + (i * pid->ki) + (d * pid->kd);
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if (isfinite(output)) {
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pid->last_output = output;
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@@ -179,7 +179,7 @@ static void
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pwm_timer_set_rate(unsigned timer, unsigned rate)
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{
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/* configure the timer to update at the desired rate */
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rARR(timer) = 1000000 / pwm_update_rate;
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rARR(timer) = 1000000 / rate;
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/* generate an update event; reloads the counter and all registers */
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rEGR(timer) = GTIM_EGR_UG;
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