fly316/PX4-Autopilot
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Lorenz Meier
2012-12-30 10:03:05 +01:00
parent b8250de1e6 62a95bf8e6
commit 142556b442
44 changed files with 2125 additions and 1308 deletions
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apps/drivers/px4fmu/fmu.cpp
+44 -5
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@@ -58,6 +58,7 @@
#include <drivers/drv_pwm_output.h>
#include <drivers/drv_gpio.h>
#include <drivers/boards/px4fmu/px4fmu_internal.h>
#include <drivers/drv_hrt.h>
#include <systemlib/systemlib.h>
#include <systemlib/err.h>
@@ -65,6 +66,7 @@
#include <drivers/drv_mixer.h>
#include <uORB/topics/actuator_controls.h>
#include <uORB/topics/actuator_controls_effective.h>
#include <uORB/topics/actuator_outputs.h>
#include <systemlib/err.h>
@@ -97,6 +99,7 @@ private:
int _t_actuators;
int _t_armed;
orb_advert_t _t_outputs;
orb_advert_t _t_actuators_effective;
unsigned _num_outputs;
bool _primary_pwm_device;
@@ -162,6 +165,7 @@ PX4FMU::PX4FMU() :
_t_actuators(-1),
_t_armed(-1),
_t_outputs(0),
_t_actuators_effective(0),
_num_outputs(0),
_primary_pwm_device(false),
_task_should_exit(false),
@@ -319,6 +323,13 @@ PX4FMU::task_main()
_t_outputs = orb_advertise(_primary_pwm_device ? ORB_ID_VEHICLE_CONTROLS : ORB_ID(actuator_outputs_1),
&outputs);
/* advertise the effective control inputs */
actuator_controls_effective_s controls_effective;
memset(&controls_effective, 0, sizeof(controls_effective));
/* advertise the effective control inputs */
_t_actuators_effective = orb_advertise(_primary_pwm_device ? ORB_ID_VEHICLE_ATTITUDE_CONTROLS_EFFECTIVE : ORB_ID(actuator_controls_effective_1),
&controls_effective);
pollfd fds[2];
fds[0].fd = _t_actuators;
fds[0].events = POLLIN;
@@ -336,8 +347,16 @@ PX4FMU::task_main()
if (_current_update_rate != _update_rate) {
int update_rate_in_ms = int(1000 / _update_rate);
if (update_rate_in_ms < 2)
/* reject faster than 500 Hz updates */
if (update_rate_in_ms < 2) {
update_rate_in_ms = 2;
_update_rate = 500;
}
/* reject slower than 50 Hz updates */
if (update_rate_in_ms > 20) {
update_rate_in_ms = 20;
_update_rate = 50;
}
orb_set_interval(_t_actuators, update_rate_in_ms);
up_pwm_servo_set_rate(_update_rate);
@@ -364,20 +383,39 @@ PX4FMU::task_main()
if (_mixers != nullptr) {
/* do mixing */
_mixers->mix(&outputs.output[0], num_outputs);
outputs.noutputs = _mixers->mix(&outputs.output[0], num_outputs);
outputs.timestamp = hrt_absolute_time();
// XXX output actual limited values
memcpy(&controls_effective, &_controls, sizeof(controls_effective));
orb_publish(_primary_pwm_device ? ORB_ID_VEHICLE_ATTITUDE_CONTROLS_EFFECTIVE : ORB_ID(actuator_controls_effective_1), _t_actuators_effective, &controls_effective);
/* iterate actuators */
for (unsigned i = 0; i < num_outputs; i++) {
/* scale for PWM output 900 - 2100us */
outputs.output[i] = 1500 + (600 * outputs.output[i]);
/* last resort: catch NaN, INF and out-of-band errors */
if (i < outputs.noutputs &&
isfinite(outputs.output[i]) &&
outputs.output[i] >= -1.0f &&
outputs.output[i] <= 1.0f) {
/* scale for PWM output 900 - 2100us */
outputs.output[i] = 1500 + (600 * outputs.output[i]);
} else {
/*
* Value is NaN, INF or out of band - set to the minimum value.
* This will be clearly visible on the servo status and will limit the risk of accidentally
* spinning motors. It would be deadly in flight.
*/
outputs.output[i] = 900;
}
/* output to the servo */
up_pwm_servo_set(i, outputs.output[i]);
}
/* and publish for anyone that cares to see */
orb_publish(ORB_ID_VEHICLE_CONTROLS, _t_outputs, &outputs);
orb_publish(_primary_pwm_device ? ORB_ID_VEHICLE_CONTROLS : ORB_ID(actuator_outputs_1), _t_outputs, &outputs);
}
}
@@ -394,6 +432,7 @@ PX4FMU::task_main()
}
::close(_t_actuators);
::close(_t_actuators_effective);
::close(_t_armed);
/* make sure servos are off */