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authorJulian Oes <joes@student.ethz.ch>2012-11-18 14:12:02 -0800
committerJulian Oes <joes@student.ethz.ch>2012-11-19 09:26:38 -0800
commit2652b16d37f2221dc9dabfa1a278651c2931e5ce (patch)
tree21614433bba8d85625c9bc996755227bbd418147 /apps/multirotor_att_control/multirotor_att_control_main.c
parent9c8e031f6be214994801a74018160174f74b5516 (diff)
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Distinction between yaw position and yaw speed control, just messsed around in the code, untested
Diffstat (limited to 'apps/multirotor_att_control/multirotor_att_control_main.c')
-rw-r--r--apps/multirotor_att_control/multirotor_att_control_main.c78
1 files changed, 50 insertions, 28 deletions
diff --git a/apps/multirotor_att_control/multirotor_att_control_main.c b/apps/multirotor_att_control/multirotor_att_control_main.c
index d2de1a787..337a45215 100644
--- a/apps/multirotor_att_control/multirotor_att_control_main.c
+++ b/apps/multirotor_att_control/multirotor_att_control_main.c
@@ -105,6 +105,7 @@ mc_thread_main(int argc, char *argv[])
memset(&rates_sp, 0, sizeof(rates_sp));
struct actuator_controls_s actuators;
+ memset(&actuators, 0, sizeof(actuators));
/* subscribe to attitude, motor setpoints and system state */
int att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
@@ -151,10 +152,14 @@ mc_thread_main(int argc, char *argv[])
bool flag_control_attitude_enabled = false;
bool flag_system_armed = false;
+ /* store if yaw position or yaw speed has been changed */
+ bool control_yaw_position = true;
+
/* prepare the handle for the failsafe throttle */
param_t failsafe_throttle_handle = param_find("MC_RCLOSS_THR");
float failsafe_throttle = 0.0f;
+
while (!thread_should_exit) {
/* wait for a sensor update, check for exit condition every 500 ms */
@@ -205,28 +210,27 @@ mc_thread_main(int argc, char *argv[])
/** STEP 1: Define which input is the dominating control input */
if (state.flag_control_offboard_enabled) {
- /* offboard inputs */
- if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_RATES) {
- rates_sp.roll = offboard_sp.p1;
- rates_sp.pitch = offboard_sp.p2;
- rates_sp.yaw = offboard_sp.p3;
- rates_sp.thrust = offboard_sp.p4;
- // printf("thrust_rate=%8.4f\n",offboard_sp.p4);
- rates_sp.timestamp = hrt_absolute_time();
- orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp);
- } else if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE) {
- att_sp.roll_body = offboard_sp.p1;
- att_sp.pitch_body = offboard_sp.p2;
- att_sp.yaw_body = offboard_sp.p3;
- att_sp.thrust = offboard_sp.p4;
- // printf("thrust_att=%8.4f\n",offboard_sp.p4);
- att_sp.timestamp = hrt_absolute_time();
- /* STEP 2: publish the result to the vehicle actuators */
- orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
- }
-
- /* decide wether we want rate or position input */
- }
+ /* offboard inputs */
+ if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_RATES) {
+ rates_sp.roll = offboard_sp.p1;
+ rates_sp.pitch = offboard_sp.p2;
+ rates_sp.yaw = offboard_sp.p3;
+ rates_sp.thrust = offboard_sp.p4;
+// printf("thrust_rate=%8.4f\n",offboard_sp.p4);
+ rates_sp.timestamp = hrt_absolute_time();
+ orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp);
+ } else if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE) {
+ att_sp.roll_body = offboard_sp.p1;
+ att_sp.pitch_body = offboard_sp.p2;
+ att_sp.yaw_body = offboard_sp.p3;
+ att_sp.thrust = offboard_sp.p4;
+// printf("thrust_att=%8.4f\n",offboard_sp.p4);
+ att_sp.timestamp = hrt_absolute_time();
+ /* STEP 2: publish the result to the vehicle actuators */
+ orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp);
+ }
+ /* decide wether we want rate or position input */
+ }
else if (state.flag_control_manual_enabled) {
/* manual inputs, from RC control or joystick */
@@ -277,14 +281,29 @@ mc_thread_main(int argc, char *argv[])
att_sp.pitch_body = manual.pitch;
/* only move setpoint if manual input is != 0 */
- // XXX turn into param
- if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.3f) {
- att_sp.yaw_body = att_sp.yaw_body + manual.yaw * 0.0025f;
- } else if (manual.throttle <= 0.3f) {
- att_sp.yaw_body = att.yaw;
+
+ if(manual.mode == MANUAL_CONTROL_MODE_ATT_YAW_POS) {
+ // XXX turn into param
+ if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.3f) {
+ att_sp.yaw_body = att_sp.yaw_body + manual.yaw * 0.0025f;
+ } else if (manual.throttle <= 0.3f) {
+ att_sp.yaw_body = att.yaw;
+ }
+ control_yaw_position = true;
+ } else if (manual.mode == MANUAL_CONTROL_MODE_ATT_YAW_RATE) {
+ if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.3f) {
+ rates_sp.yaw = manual.yaw;
+ control_yaw_position = false;
+ } else {
+ att_sp.yaw_body = 0.0f;
+ control_yaw_position = true;
+ }
}
+
att_sp.thrust = manual.throttle;
att_sp.timestamp = hrt_absolute_time();
+
+ //rates_sp.yaw = manual.yaw;
}
}
/* STEP 2: publish the result to the vehicle actuators */
@@ -305,7 +324,10 @@ mc_thread_main(int argc, char *argv[])
/** STEP 3: Identify the controller setup to run and set up the inputs correctly */
if (state.flag_control_attitude_enabled) {
- multirotor_control_attitude(&att_sp, &att, &rates_sp, NULL);
+ multirotor_control_attitude(&att_sp, &att, &rates_sp, NULL, control_yaw_position);
+
+
+
orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp);
}