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authorLorenz Meier <lm@inf.ethz.ch>2012-09-19 18:53:29 +0200
committerLorenz Meier <lm@inf.ethz.ch>2012-09-19 18:53:29 +0200
commit291f4f3a33e6428b23624b1ffe12fec1015816cd (patch)
tree0dc7b590081184d46ffa2ad88ba6fbe56a364891 /apps/multirotor_att_control
parentb0b72b11eb6c112d3fb58385f5681af55dd5605a (diff)
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Reworked control interface, needs testing / validation
Diffstat (limited to 'apps/multirotor_att_control')
-rw-r--r--apps/multirotor_att_control/multirotor_att_control_main.c31
-rw-r--r--apps/multirotor_att_control/multirotor_attitude_control.c2
-rw-r--r--apps/multirotor_att_control/multirotor_rate_control.c8
-rw-r--r--apps/multirotor_att_control/multirotor_rate_control.h4
4 files changed, 29 insertions, 16 deletions
diff --git a/apps/multirotor_att_control/multirotor_att_control_main.c b/apps/multirotor_att_control/multirotor_att_control_main.c
index 530033701..3f0d56245 100644
--- a/apps/multirotor_att_control/multirotor_att_control_main.c
+++ b/apps/multirotor_att_control/multirotor_att_control_main.c
@@ -58,13 +58,14 @@
#include <uORB/topics/vehicle_attitude.h>
#include <uORB/topics/vehicle_attitude_setpoint.h>
#include <uORB/topics/manual_control_setpoint.h>
-#include <uORB/topics/ardrone_motors_setpoint.h>
+#include <uORB/topics/vehicle_rates_setpoint.h>
#include <uORB/topics/sensor_combined.h>
#include <uORB/topics/actuator_controls.h>
#include <systemlib/perf_counter.h>
#include "multirotor_attitude_control.h"
+#include "multirotor_rate_control.h"
__EXPORT int multirotor_att_control_main(int argc, char *argv[]);
@@ -93,18 +94,18 @@ mc_thread_main(int argc, char *argv[])
memset(&manual, 0, sizeof(manual));
struct sensor_combined_s raw;
memset(&raw, 0, sizeof(raw));
- struct ardrone_motors_setpoint_s setpoint;
- memset(&setpoint, 0, sizeof(setpoint));
+ struct vehicle_rates_setpoint_s rates_sp;
+ memset(&rates_sp, 0, sizeof(rates_sp));
struct actuator_controls_s actuators;
/* subscribe to attitude, motor setpoints and system state */
int att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
int att_setpoint_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint));
+ int setpoint_sub = orb_subscribe(ORB_ID(vehicle_rates_setpoint));
int state_sub = orb_subscribe(ORB_ID(vehicle_status));
int manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
int sensor_sub = orb_subscribe(ORB_ID(sensor_combined));
- int setpoint_sub = orb_subscribe(ORB_ID(ardrone_motors_setpoint));
/*
* Do not rate-limit the loop to prevent aliasing
@@ -145,6 +146,12 @@ mc_thread_main(int argc, char *argv[])
orb_copy(ORB_ID(vehicle_attitude), att_sub, &att);
/* get a local copy of attitude setpoint */
orb_copy(ORB_ID(vehicle_attitude_setpoint), att_setpoint_sub, &att_sp);
+ /* get a local copy of rates setpoint */
+ bool updated;
+ orb_check(setpoint_sub, &updated);
+ if (updated) {
+ orb_copy(ORB_ID(vehicle_rates_setpoint), setpoint_sub, &rates_sp);
+ }
/* get a local copy of the current sensor values */
orb_copy(ORB_ID(sensor_combined), sensor_sub, &raw);
@@ -155,16 +162,15 @@ mc_thread_main(int argc, char *argv[])
/* manual inputs, from RC control or joystick */
att_sp.roll_body = manual.roll;
att_sp.pitch_body = manual.pitch;
- att_sp.yaw_rate_body = manual.yaw;
+ att_sp.yaw_body = manual.yaw; // XXX Hack, remove, switch to yaw rate controller
+ /* set yaw rate */
+ rates_sp.yaw = manual.yaw;
att_sp.timestamp = hrt_absolute_time();
if (motor_test_mode) {
att_sp.roll_body = 0.0f;
att_sp.pitch_body = 0.0f;
att_sp.yaw_body = 0.0f;
- att_sp.roll_rate_body = 0.0f;
- att_sp.pitch_rate_body = 0.0f;
- att_sp.yaw_rate_body = 0.0f;
att_sp.thrust = 0.1f;
} else {
att_sp.thrust = manual.throttle;
@@ -184,7 +190,14 @@ mc_thread_main(int argc, char *argv[])
/* XXX could be also run in an independent loop */
if (state.flag_control_rates_enabled) {
- multirotor_control_rates(&att_sp, &raw.gyro_rad_s, &actuators);
+ /* lowpass gyros */
+ // XXX
+ static float gyro_lp[3] = {0, 0, 0};
+ gyro_lp[0] = raw.gyro_rad_s[0];
+ gyro_lp[1] = raw.gyro_rad_s[1];
+ gyro_lp[2] = raw.gyro_rad_s[2];
+
+ multirotor_control_rates(&rates_sp, gyro_lp, &actuators);
}
/* STEP 3: publish the result to the vehicle actuators */
diff --git a/apps/multirotor_att_control/multirotor_attitude_control.c b/apps/multirotor_att_control/multirotor_attitude_control.c
index 997aa0c10..d7413913b 100644
--- a/apps/multirotor_att_control/multirotor_attitude_control.c
+++ b/apps/multirotor_att_control/multirotor_attitude_control.c
@@ -243,7 +243,7 @@ void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_s
float roll_control = pid_calculate(&roll_controller, att_sp->roll_body + p.att_yoff,
att->roll, att->rollspeed, deltaT);
/* control yaw rate */
- float yaw_rate_control = pid_calculate(&yaw_speed_controller, att_sp->yaw_rate_body, att->yawspeed, 0.0f, deltaT);
+ float yaw_rate_control = pid_calculate(&yaw_speed_controller, att_sp->yaw_body, att->yawspeed, 0.0f, deltaT);
/*
* compensate the vertical loss of thrust
diff --git a/apps/multirotor_att_control/multirotor_rate_control.c b/apps/multirotor_att_control/multirotor_rate_control.c
index 8a3ac78cd..fefd1f767 100644
--- a/apps/multirotor_att_control/multirotor_rate_control.c
+++ b/apps/multirotor_att_control/multirotor_rate_control.c
@@ -132,7 +132,7 @@ static int parameters_update(const struct mc_rate_control_param_handles *h, stru
return OK;
}
-void multirotor_control_rates(const struct vehicle_attitude_setpoint_s *rate_sp,
+void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp,
const float rates[], struct actuator_controls_s *actuators)
{
static uint64_t last_run = 0;
@@ -179,13 +179,13 @@ void multirotor_control_rates(const struct vehicle_attitude_setpoint_s *rate_sp,
/* calculate current control outputs */
/* control pitch (forward) output */
- float pitch_control = pid_calculate(&pitch_controller, rate_sp->pitch_rate_body,
+ float pitch_control = pid_calculate(&pitch_controller, rate_sp->pitch,
rates[1], 0.0f, deltaT);
/* control roll (left/right) output */
- float roll_control = pid_calculate(&roll_controller, rate_sp->roll_rate_body,
+ float roll_control = pid_calculate(&roll_controller, rate_sp->roll,
rates[0], 0.0f, deltaT);
/* control yaw rate */
- float yaw_rate_control = pid_calculate(&yaw_speed_controller, rate_sp->yaw_rate_body, rates[2], 0.0f, deltaT);
+ float yaw_rate_control = pid_calculate(&yaw_speed_controller, rate_sp->yaw, rates[2], 0.0f, deltaT);
/*
* compensate the vertical loss of thrust
diff --git a/apps/multirotor_att_control/multirotor_rate_control.h b/apps/multirotor_att_control/multirotor_rate_control.h
index 6f34d99e7..3c3c50801 100644
--- a/apps/multirotor_att_control/multirotor_rate_control.h
+++ b/apps/multirotor_att_control/multirotor_rate_control.h
@@ -47,10 +47,10 @@
#include <uORB/uORB.h>
#include <uORB/topics/vehicle_attitude.h>
-#include <uORB/topics/vehicle_attitude_setpoint.h>
+#include <uORB/topics/vehicle_rates_setpoint.h>
#include <uORB/topics/actuator_controls.h>
-void multirotor_control_rates(const struct vehicle_attitude_setpoint_s *rate_sp,
+void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp,
const float rates[], struct actuator_controls_s *actuators);
#endif /* MULTIROTOR_RATE_CONTROL_H_ */