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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-15 18:23:34 +08:00
Merge remote-tracking branch 'upstream/master' into dev_ros
This commit is contained in:
@@ -1405,7 +1405,7 @@ Mavlink::task_main(int argc, char *argv[])
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configure_stream("POSITION_TARGET_GLOBAL_INT", 3.0f);
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configure_stream("ATTITUDE_TARGET", 3.0f);
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configure_stream("DISTANCE_SENSOR", 0.5f);
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configure_stream("OPTICAL_FLOW", 5.0f);
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configure_stream("OPTICAL_FLOW_RAD", 5.0f);
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break;
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case MAVLINK_MODE_ONBOARD:
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@@ -1834,33 +1834,32 @@ protected:
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}
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};
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class MavlinkStreamOpticalFlow : public MavlinkStream
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class MavlinkStreamOpticalFlowRad : public MavlinkStream
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{
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public:
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const char *get_name() const
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{
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return MavlinkStreamOpticalFlow::get_name_static();
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return MavlinkStreamOpticalFlowRad::get_name_static();
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}
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static const char *get_name_static()
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{
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return "OPTICAL_FLOW";
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return "OPTICAL_FLOW_RAD";
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}
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uint8_t get_id()
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{
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return MAVLINK_MSG_ID_OPTICAL_FLOW;
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return MAVLINK_MSG_ID_OPTICAL_FLOW_RAD;
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}
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static MavlinkStream *new_instance(Mavlink *mavlink)
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{
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return new MavlinkStreamOpticalFlow(mavlink);
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return new MavlinkStreamOpticalFlowRad(mavlink);
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}
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unsigned get_size()
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{
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return _flow_sub->is_published() ? (MAVLINK_MSG_ID_OPTICAL_FLOW_LEN + MAVLINK_NUM_NON_PAYLOAD_BYTES) : 0;
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return _flow_sub->is_published() ? (MAVLINK_MSG_ID_OPTICAL_FLOW_RAD_LEN + MAVLINK_NUM_NON_PAYLOAD_BYTES) : 0;
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}
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private:
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@@ -1868,11 +1867,11 @@ private:
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uint64_t _flow_time;
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/* do not allow top copying this class */
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MavlinkStreamOpticalFlow(MavlinkStreamOpticalFlow &);
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MavlinkStreamOpticalFlow& operator = (const MavlinkStreamOpticalFlow &);
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MavlinkStreamOpticalFlowRad(MavlinkStreamOpticalFlowRad &);
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MavlinkStreamOpticalFlowRad& operator = (const MavlinkStreamOpticalFlowRad &);
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protected:
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explicit MavlinkStreamOpticalFlow(Mavlink *mavlink) : MavlinkStream(mavlink),
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explicit MavlinkStreamOpticalFlowRad(Mavlink *mavlink) : MavlinkStream(mavlink),
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_flow_sub(_mavlink->add_orb_subscription(ORB_ID(optical_flow))),
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_flow_time(0)
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{}
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@@ -1882,18 +1881,23 @@ protected:
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struct optical_flow_s flow;
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if (_flow_sub->update(&_flow_time, &flow)) {
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mavlink_optical_flow_t msg;
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mavlink_optical_flow_rad_t msg;
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msg.time_usec = flow.timestamp;
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msg.sensor_id = flow.sensor_id;
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msg.flow_x = flow.flow_raw_x;
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msg.flow_y = flow.flow_raw_y;
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msg.flow_comp_m_x = flow.flow_comp_x_m;
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msg.flow_comp_m_y = flow.flow_comp_y_m;
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msg.integrated_x = flow.pixel_flow_x_integral;
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msg.integrated_y = flow.pixel_flow_y_integral;
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msg.integrated_xgyro = flow.gyro_x_rate_integral;
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msg.integrated_ygyro = flow.gyro_y_rate_integral;
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msg.integrated_zgyro = flow.gyro_z_rate_integral;
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msg.distance = flow.ground_distance_m;
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msg.quality = flow.quality;
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msg.ground_distance = flow.ground_distance_m;
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msg.integration_time_us = flow.integration_timespan;
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msg.sensor_id = flow.sensor_id;
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msg.time_delta_distance_us = flow.time_since_last_sonar_update;
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msg.temperature = flow.gyro_temperature;
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_mavlink->send_message(MAVLINK_MSG_ID_OPTICAL_FLOW, &msg);
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_mavlink->send_message(MAVLINK_MSG_ID_OPTICAL_FLOW_RAD, &msg);
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}
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}
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};
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@@ -2199,7 +2203,7 @@ StreamListItem *streams_list[] = {
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new StreamListItem(&MavlinkStreamAttitudeTarget::new_instance, &MavlinkStreamAttitudeTarget::get_name_static),
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new StreamListItem(&MavlinkStreamRCChannelsRaw::new_instance, &MavlinkStreamRCChannelsRaw::get_name_static),
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new StreamListItem(&MavlinkStreamManualControl::new_instance, &MavlinkStreamManualControl::get_name_static),
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new StreamListItem(&MavlinkStreamOpticalFlow::new_instance, &MavlinkStreamOpticalFlow::get_name_static),
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new StreamListItem(&MavlinkStreamOpticalFlowRad::new_instance, &MavlinkStreamOpticalFlowRad::get_name_static),
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new StreamListItem(&MavlinkStreamAttitudeControls::new_instance, &MavlinkStreamAttitudeControls::get_name_static),
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new StreamListItem(&MavlinkStreamNamedValueFloat::new_instance, &MavlinkStreamNamedValueFloat::get_name_static),
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new StreamListItem(&MavlinkStreamCameraCapture::new_instance, &MavlinkStreamCameraCapture::get_name_static),
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||||
@@ -144,8 +144,8 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg)
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||||
handle_message_command_int(msg);
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break;
|
||||
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||||
case MAVLINK_MSG_ID_OPTICAL_FLOW:
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handle_message_optical_flow(msg);
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case MAVLINK_MSG_ID_OPTICAL_FLOW_RAD:
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handle_message_optical_flow_rad(msg);
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break;
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||||
case MAVLINK_MSG_ID_SET_MODE:
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||||
@@ -352,24 +352,27 @@ MavlinkReceiver::handle_message_command_int(mavlink_message_t *msg)
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||||
}
|
||||
|
||||
void
|
||||
MavlinkReceiver::handle_message_optical_flow(mavlink_message_t *msg)
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MavlinkReceiver::handle_message_optical_flow_rad(mavlink_message_t *msg)
|
||||
{
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||||
/* optical flow */
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mavlink_optical_flow_t flow;
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mavlink_msg_optical_flow_decode(msg, &flow);
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mavlink_optical_flow_rad_t flow;
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mavlink_msg_optical_flow_rad_decode(msg, &flow);
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struct optical_flow_s f;
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||||
memset(&f, 0, sizeof(f));
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|
||||
f.timestamp = hrt_absolute_time();
|
||||
f.flow_timestamp = flow.time_usec;
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||||
f.flow_raw_x = flow.flow_x;
|
||||
f.flow_raw_y = flow.flow_y;
|
||||
f.flow_comp_x_m = flow.flow_comp_m_x;
|
||||
f.flow_comp_y_m = flow.flow_comp_m_y;
|
||||
f.ground_distance_m = flow.ground_distance;
|
||||
f.timestamp = flow.time_usec;
|
||||
f.integration_timespan = flow.integration_time_us;
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||||
f.pixel_flow_x_integral = flow.integrated_x;
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||||
f.pixel_flow_y_integral = flow.integrated_y;
|
||||
f.gyro_x_rate_integral = flow.integrated_xgyro;
|
||||
f.gyro_y_rate_integral = flow.integrated_ygyro;
|
||||
f.gyro_z_rate_integral = flow.integrated_zgyro;
|
||||
f.time_since_last_sonar_update = flow.time_delta_distance_us;
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||||
f.ground_distance_m = flow.distance;
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||||
f.quality = flow.quality;
|
||||
f.sensor_id = flow.sensor_id;
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||||
f.gyro_temperature = flow.temperature;
|
||||
|
||||
if (_flow_pub < 0) {
|
||||
_flow_pub = orb_advertise(ORB_ID(optical_flow), &f);
|
||||
@@ -389,13 +392,18 @@ MavlinkReceiver::handle_message_hil_optical_flow(mavlink_message_t *msg)
|
||||
struct optical_flow_s f;
|
||||
memset(&f, 0, sizeof(f));
|
||||
|
||||
f.timestamp = hrt_absolute_time();
|
||||
f.flow_timestamp = flow.time_usec;
|
||||
f.flow_raw_x = flow.integrated_x;
|
||||
f.flow_raw_y = flow.integrated_y;
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f.timestamp = hrt_absolute_time(); // XXX we rely on the system time for now and not flow.time_usec;
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f.integration_timespan = flow.integration_time_us;
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f.pixel_flow_x_integral = flow.integrated_x;
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f.pixel_flow_y_integral = flow.integrated_y;
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f.gyro_x_rate_integral = flow.integrated_xgyro;
|
||||
f.gyro_y_rate_integral = flow.integrated_ygyro;
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f.gyro_z_rate_integral = flow.integrated_zgyro;
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||||
f.time_since_last_sonar_update = flow.time_delta_distance_us;
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||||
f.ground_distance_m = flow.distance;
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f.quality = flow.quality;
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||||
f.sensor_id = flow.sensor_id;
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f.gyro_temperature = flow.temperature;
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if (_flow_pub < 0) {
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_flow_pub = orb_advertise(ORB_ID(optical_flow), &f);
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@@ -112,7 +112,7 @@ private:
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void handle_message(mavlink_message_t *msg);
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void handle_message_command_long(mavlink_message_t *msg);
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void handle_message_command_int(mavlink_message_t *msg);
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void handle_message_optical_flow(mavlink_message_t *msg);
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void handle_message_optical_flow_rad(mavlink_message_t *msg);
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void handle_message_hil_optical_flow(mavlink_message_t *msg);
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void handle_message_set_mode(mavlink_message_t *msg);
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void handle_message_vicon_position_estimate(mavlink_message_t *msg);
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||||
@@ -296,7 +296,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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float w_flow = 0.0f;
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||||
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||||
float sonar_prev = 0.0f;
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||||
hrt_abstime flow_prev = 0; // time of last flow measurement
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//hrt_abstime flow_prev = 0; // time of last flow measurement
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hrt_abstime sonar_time = 0; // time of last sonar measurement (not filtered)
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hrt_abstime sonar_valid_time = 0; // time of last sonar measurement used for correction (filtered)
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@@ -489,8 +489,8 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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orb_copy(ORB_ID(optical_flow), optical_flow_sub, &flow);
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/* calculate time from previous update */
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float flow_dt = flow_prev > 0 ? (flow.flow_timestamp - flow_prev) * 1e-6f : 0.1f;
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flow_prev = flow.flow_timestamp;
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// float flow_dt = flow_prev > 0 ? (flow.flow_timestamp - flow_prev) * 1e-6f : 0.1f;
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// flow_prev = flow.flow_timestamp;
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if ((flow.ground_distance_m > 0.31f) &&
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(flow.ground_distance_m < 4.0f) &&
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@@ -548,8 +548,9 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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||||
|
||||
/* convert raw flow to angular flow (rad/s) */
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float flow_ang[2];
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flow_ang[0] = flow.flow_raw_x * params.flow_k / 1000.0f / flow_dt;
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flow_ang[1] = flow.flow_raw_y * params.flow_k / 1000.0f / flow_dt;
|
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//todo check direction of x und y axis
|
||||
flow_ang[0] = flow.pixel_flow_x_integral/(float)flow.integration_timespan*1000000.0f;//flow.flow_raw_x * params.flow_k / 1000.0f / flow_dt;
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||||
flow_ang[1] = flow.pixel_flow_y_integral/(float)flow.integration_timespan*1000000.0f;//flow.flow_raw_y * params.flow_k / 1000.0f / flow_dt;
|
||||
/* flow measurements vector */
|
||||
float flow_m[3];
|
||||
flow_m[0] = -flow_ang[0] * flow_dist;
|
||||
|
||||
@@ -412,7 +412,6 @@ registers_set(uint8_t page, uint8_t offset, const uint16_t *values, unsigned num
|
||||
* text handling function.
|
||||
*/
|
||||
return mixer_handle_text(values, num_values * sizeof(*values));
|
||||
break;
|
||||
|
||||
default:
|
||||
/* avoid offset wrap */
|
||||
@@ -584,10 +583,7 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
|
||||
break;
|
||||
|
||||
case PX4IO_P_SETUP_REBOOT_BL:
|
||||
// do not reboot if FMU is armed and IO's safety is off
|
||||
// this state defines an active system.
|
||||
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) &&
|
||||
(r_status_flags & PX4IO_P_SETUP_ARMING_FMU_ARMED)) {
|
||||
if (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) {
|
||||
// don't allow reboot while armed
|
||||
break;
|
||||
}
|
||||
@@ -633,12 +629,9 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
|
||||
case PX4IO_PAGE_RC_CONFIG: {
|
||||
|
||||
/**
|
||||
* do not allow a RC config change while outputs armed
|
||||
* = FMU is armed and IO's safety is off
|
||||
* this state defines an active system.
|
||||
* do not allow a RC config change while safety is off
|
||||
*/
|
||||
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) &&
|
||||
(r_status_flags & PX4IO_P_SETUP_ARMING_FMU_ARMED)) {
|
||||
if (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) {
|
||||
break;
|
||||
}
|
||||
|
||||
|
||||
@@ -1518,11 +1518,14 @@ int sdlog2_thread_main(int argc, char *argv[])
|
||||
/* --- FLOW --- */
|
||||
if (copy_if_updated(ORB_ID(optical_flow), subs.flow_sub, &buf.flow)) {
|
||||
log_msg.msg_type = LOG_FLOW_MSG;
|
||||
log_msg.body.log_FLOW.flow_raw_x = buf.flow.flow_raw_x;
|
||||
log_msg.body.log_FLOW.flow_raw_y = buf.flow.flow_raw_y;
|
||||
log_msg.body.log_FLOW.flow_comp_x = buf.flow.flow_comp_x_m;
|
||||
log_msg.body.log_FLOW.flow_comp_y = buf.flow.flow_comp_y_m;
|
||||
log_msg.body.log_FLOW.distance = buf.flow.ground_distance_m;
|
||||
log_msg.body.log_FLOW.ground_distance_m = buf.flow.ground_distance_m;
|
||||
log_msg.body.log_FLOW.gyro_temperature = buf.flow.gyro_temperature;
|
||||
log_msg.body.log_FLOW.gyro_x_rate_integral = buf.flow.gyro_x_rate_integral;
|
||||
log_msg.body.log_FLOW.gyro_y_rate_integral = buf.flow.gyro_y_rate_integral;
|
||||
log_msg.body.log_FLOW.gyro_z_rate_integral = buf.flow.gyro_z_rate_integral;
|
||||
log_msg.body.log_FLOW.integration_timespan = buf.flow.integration_timespan;
|
||||
log_msg.body.log_FLOW.pixel_flow_x_integral = buf.flow.pixel_flow_x_integral;
|
||||
log_msg.body.log_FLOW.pixel_flow_y_integral = buf.flow.pixel_flow_y_integral;
|
||||
log_msg.body.log_FLOW.quality = buf.flow.quality;
|
||||
log_msg.body.log_FLOW.sensor_id = buf.flow.sensor_id;
|
||||
LOGBUFFER_WRITE_AND_COUNT(FLOW);
|
||||
|
||||
@@ -200,13 +200,19 @@ struct log_ARSP_s {
|
||||
/* --- FLOW - OPTICAL FLOW --- */
|
||||
#define LOG_FLOW_MSG 15
|
||||
struct log_FLOW_s {
|
||||
int16_t flow_raw_x;
|
||||
int16_t flow_raw_y;
|
||||
float flow_comp_x;
|
||||
float flow_comp_y;
|
||||
float distance;
|
||||
uint8_t quality;
|
||||
uint64_t timestamp;
|
||||
uint8_t sensor_id;
|
||||
float pixel_flow_x_integral;
|
||||
float pixel_flow_y_integral;
|
||||
float gyro_x_rate_integral;
|
||||
float gyro_y_rate_integral;
|
||||
float gyro_z_rate_integral;
|
||||
float ground_distance_m;
|
||||
uint32_t integration_timespan;
|
||||
uint32_t time_since_last_sonar_update;
|
||||
uint16_t frame_count_since_last_readout;
|
||||
int16_t gyro_temperature;
|
||||
uint8_t quality;
|
||||
};
|
||||
|
||||
/* --- GPOS - GLOBAL POSITION ESTIMATE --- */
|
||||
|
||||
@@ -46,6 +46,7 @@
|
||||
#include "topics/vehicle_attitude_setpoint.h"
|
||||
#include "topics/vehicle_rates_setpoint.h"
|
||||
#include "topics/actuator_outputs.h"
|
||||
#include "topics/actuator_direct.h"
|
||||
#include "topics/encoders.h"
|
||||
#include "topics/tecs_status.h"
|
||||
#include "topics/rc_channels.h"
|
||||
@@ -77,6 +78,7 @@ template class __EXPORT Publication<vehicle_global_velocity_setpoint_s>;
|
||||
template class __EXPORT Publication<vehicle_attitude_setpoint_s>;
|
||||
template class __EXPORT Publication<vehicle_rates_setpoint_s>;
|
||||
template class __EXPORT Publication<actuator_outputs_s>;
|
||||
template class __EXPORT Publication<actuator_direct_s>;
|
||||
template class __EXPORT Publication<encoders_s>;
|
||||
template class __EXPORT Publication<tecs_status_s>;
|
||||
template class __EXPORT Publication<rc_channels_s>;
|
||||
|
||||
@@ -192,6 +192,9 @@ ORB_DEFINE(actuator_outputs_1, struct actuator_outputs_s);
|
||||
ORB_DEFINE(actuator_outputs_2, struct actuator_outputs_s);
|
||||
ORB_DEFINE(actuator_outputs_3, struct actuator_outputs_s);
|
||||
|
||||
#include "topics/actuator_direct.h"
|
||||
ORB_DEFINE(actuator_direct, struct actuator_direct_s);
|
||||
|
||||
#include "topics/multirotor_motor_limits.h"
|
||||
ORB_DEFINE(multirotor_motor_limits, struct multirotor_motor_limits_s);
|
||||
|
||||
|
||||
@@ -0,0 +1,69 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
|
||||
*
|
||||
* Redistribution and use in source and binary forms, with or without
|
||||
* modification, are permitted provided that the following conditions
|
||||
* are met:
|
||||
*
|
||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
|
||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* the documentation and/or other materials provided with the
|
||||
* distribution.
|
||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||
* used to endorse or promote products derived from this software
|
||||
* without specific prior written permission.
|
||||
*
|
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
* POSSIBILITY OF SUCH DAMAGE.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
/**
|
||||
* @file actuator_direct.h
|
||||
*
|
||||
* Actuator direct values.
|
||||
*
|
||||
* Values published to this topic are the direct actuator values which
|
||||
* should be passed to actuators, bypassing mixing
|
||||
*/
|
||||
|
||||
#ifndef TOPIC_ACTUATOR_DIRECT_H
|
||||
#define TOPIC_ACTUATOR_DIRECT_H
|
||||
|
||||
#include <stdint.h>
|
||||
#include "../uORB.h"
|
||||
|
||||
#define NUM_ACTUATORS_DIRECT 16
|
||||
|
||||
/**
|
||||
* @addtogroup topics
|
||||
* @{
|
||||
*/
|
||||
|
||||
struct actuator_direct_s {
|
||||
uint64_t timestamp; /**< timestamp in us since system boot */
|
||||
float values[NUM_ACTUATORS_DIRECT]; /**< actuator values, from -1 to 1 */
|
||||
unsigned nvalues; /**< number of valid values */
|
||||
};
|
||||
|
||||
/**
|
||||
* @}
|
||||
*/
|
||||
|
||||
/* actuator direct ORB */
|
||||
ORB_DECLARE(actuator_direct);
|
||||
|
||||
#endif // TOPIC_ACTUATOR_DIRECT_H
|
||||
@@ -55,16 +55,22 @@
|
||||
*/
|
||||
struct optical_flow_s {
|
||||
|
||||
uint64_t timestamp; /**< in microseconds since system start */
|
||||
|
||||
uint64_t flow_timestamp; /**< timestamp from flow sensor */
|
||||
int16_t flow_raw_x; /**< flow in pixels in X direction, not rotation-compensated */
|
||||
int16_t flow_raw_y; /**< flow in pixels in Y direction, not rotation-compensated */
|
||||
float flow_comp_x_m; /**< speed over ground in meters, rotation-compensated */
|
||||
float flow_comp_y_m; /**< speed over ground in meters, rotation-compensated */
|
||||
float ground_distance_m; /**< Altitude / distance to ground in meters */
|
||||
uint8_t quality; /**< Quality of the measurement, 0: bad quality, 255: maximum quality */
|
||||
uint64_t timestamp; /**< in microseconds since system start */
|
||||
uint8_t sensor_id; /**< id of the sensor emitting the flow value */
|
||||
float pixel_flow_x_integral; /**< accumulated optical flow in radians around x axis */
|
||||
float pixel_flow_y_integral; /**< accumulated optical flow in radians around y axis */
|
||||
float gyro_x_rate_integral; /**< accumulated gyro value in radians around x axis */
|
||||
float gyro_y_rate_integral; /**< accumulated gyro value in radians around y axis */
|
||||
float gyro_z_rate_integral; /**< accumulated gyro value in radians around z axis */
|
||||
float ground_distance_m; /**< Altitude / distance to ground in meters */
|
||||
uint32_t integration_timespan; /**<accumulation timespan in microseconds */
|
||||
uint32_t time_since_last_sonar_update;/**< time since last sonar update in microseconds */
|
||||
uint16_t frame_count_since_last_readout;/**< number of accumulated frames in timespan */
|
||||
int16_t gyro_temperature;/**< Temperature * 100 in centi-degrees Celsius */
|
||||
uint8_t quality; /**< Average of quality of accumulated frames, 0: bad quality, 255: maximum quality */
|
||||
|
||||
|
||||
|
||||
|
||||
};
|
||||
|
||||
|
||||
@@ -76,7 +76,9 @@ int UavcanEscController::init()
|
||||
|
||||
void UavcanEscController::update_outputs(float *outputs, unsigned num_outputs)
|
||||
{
|
||||
if ((outputs == nullptr) || (num_outputs > uavcan::equipment::esc::RawCommand::FieldTypes::cmd::MaxSize)) {
|
||||
if ((outputs == nullptr) ||
|
||||
(num_outputs > uavcan::equipment::esc::RawCommand::FieldTypes::cmd::MaxSize) ||
|
||||
(num_outputs > CONNECTED_ESC_MAX)) {
|
||||
perf_count(_perfcnt_invalid_input);
|
||||
return;
|
||||
}
|
||||
@@ -101,10 +103,15 @@ void UavcanEscController::update_outputs(float *outputs, unsigned num_outputs)
|
||||
for (unsigned i = 0; i < num_outputs; i++) {
|
||||
if (_armed_mask & MOTOR_BIT(i)) {
|
||||
float scaled = (outputs[i] + 1.0F) * 0.5F * cmd_max;
|
||||
if (scaled < 1.0F) {
|
||||
scaled = 1.0F; // Since we're armed, we don't want to stop it completely
|
||||
}
|
||||
|
||||
// trim negative values back to 0. Previously
|
||||
// we set this to 0.1, which meant motors kept
|
||||
// spinning when armed, but that should be a
|
||||
// policy decision for a specific vehicle
|
||||
// type, as it is not appropriate for all
|
||||
// types of vehicles (eg. fixed wing).
|
||||
if (scaled < 0.0F) {
|
||||
scaled = 0.0F;
|
||||
}
|
||||
if (scaled > cmd_max) {
|
||||
scaled = cmd_max;
|
||||
perf_count(_perfcnt_scaling_error);
|
||||
|
||||
@@ -269,6 +269,24 @@ void UavcanNode::node_spin_once()
|
||||
}
|
||||
}
|
||||
|
||||
/*
|
||||
add a fd to the list of polled events. This assumes you want
|
||||
POLLIN for now.
|
||||
*/
|
||||
int UavcanNode::add_poll_fd(int fd)
|
||||
{
|
||||
int ret = _poll_fds_num;
|
||||
if (_poll_fds_num >= UAVCAN_NUM_POLL_FDS) {
|
||||
errx(1, "uavcan: too many poll fds, exiting");
|
||||
}
|
||||
_poll_fds[_poll_fds_num] = ::pollfd();
|
||||
_poll_fds[_poll_fds_num].fd = fd;
|
||||
_poll_fds[_poll_fds_num].events = POLLIN;
|
||||
_poll_fds_num += 1;
|
||||
return ret;
|
||||
}
|
||||
|
||||
|
||||
int UavcanNode::run()
|
||||
{
|
||||
(void)pthread_mutex_lock(&_node_mutex);
|
||||
@@ -280,9 +298,9 @@ int UavcanNode::run()
|
||||
|
||||
_armed_sub = orb_subscribe(ORB_ID(actuator_armed));
|
||||
_test_motor_sub = orb_subscribe(ORB_ID(test_motor));
|
||||
_actuator_direct_sub = orb_subscribe(ORB_ID(actuator_direct));
|
||||
|
||||
actuator_outputs_s outputs;
|
||||
memset(&outputs, 0, sizeof(outputs));
|
||||
memset(&_outputs, 0, sizeof(_outputs));
|
||||
|
||||
const int busevent_fd = ::open(uavcan_stm32::BusEvent::DevName, 0);
|
||||
if (busevent_fd < 0)
|
||||
@@ -304,11 +322,15 @@ int UavcanNode::run()
|
||||
* the value returned from poll() to detect whether actuator control has timed out or not.
|
||||
* Instead, all ORB events need to be checked individually (see below).
|
||||
*/
|
||||
_poll_fds_num = 0;
|
||||
_poll_fds[_poll_fds_num] = ::pollfd();
|
||||
_poll_fds[_poll_fds_num].fd = busevent_fd;
|
||||
_poll_fds[_poll_fds_num].events = POLLIN;
|
||||
_poll_fds_num += 1;
|
||||
add_poll_fd(busevent_fd);
|
||||
|
||||
/*
|
||||
* setup poll to look for actuator direct input if we are
|
||||
* subscribed to the topic
|
||||
*/
|
||||
if (_actuator_direct_sub != -1) {
|
||||
_actuator_direct_poll_fd_num = add_poll_fd(_actuator_direct_sub);
|
||||
}
|
||||
|
||||
while (!_task_should_exit) {
|
||||
// update actuator controls subscriptions if needed
|
||||
@@ -326,6 +348,8 @@ int UavcanNode::run()
|
||||
|
||||
node_spin_once(); // Non-blocking
|
||||
|
||||
bool new_output = false;
|
||||
|
||||
// this would be bad...
|
||||
if (poll_ret < 0) {
|
||||
log("poll error %d", errno);
|
||||
@@ -333,24 +357,39 @@ int UavcanNode::run()
|
||||
} else {
|
||||
// get controls for required topics
|
||||
bool controls_updated = false;
|
||||
unsigned poll_id = 1;
|
||||
for (unsigned i = 0; i < NUM_ACTUATOR_CONTROL_GROUPS; i++) {
|
||||
if (_control_subs[i] > 0) {
|
||||
if (_poll_fds[poll_id].revents & POLLIN) {
|
||||
if (_poll_fds[_poll_ids[i]].revents & POLLIN) {
|
||||
controls_updated = true;
|
||||
orb_copy(_control_topics[i], _control_subs[i], &_controls[i]);
|
||||
}
|
||||
poll_id++;
|
||||
}
|
||||
}
|
||||
|
||||
/*
|
||||
see if we have any direct actuator updates
|
||||
*/
|
||||
if (_actuator_direct_sub != -1 &&
|
||||
(_poll_fds[_actuator_direct_poll_fd_num].revents & POLLIN) &&
|
||||
orb_copy(ORB_ID(actuator_direct), _actuator_direct_sub, &_actuator_direct) == OK &&
|
||||
!_test_in_progress) {
|
||||
if (_actuator_direct.nvalues > NUM_ACTUATOR_OUTPUTS) {
|
||||
_actuator_direct.nvalues = NUM_ACTUATOR_OUTPUTS;
|
||||
}
|
||||
memcpy(&_outputs.output[0], &_actuator_direct.values[0],
|
||||
_actuator_direct.nvalues*sizeof(float));
|
||||
_outputs.noutputs = _actuator_direct.nvalues;
|
||||
new_output = true;
|
||||
}
|
||||
|
||||
// can we mix?
|
||||
if (_test_in_progress) {
|
||||
float test_outputs[NUM_ACTUATOR_OUTPUTS] = {};
|
||||
test_outputs[_test_motor.motor_number] = _test_motor.value*2.0f-1.0f;
|
||||
|
||||
// Output to the bus
|
||||
_esc_controller.update_outputs(test_outputs, NUM_ACTUATOR_OUTPUTS);
|
||||
memset(&_outputs, 0, sizeof(_outputs));
|
||||
if (_test_motor.motor_number < NUM_ACTUATOR_OUTPUTS) {
|
||||
_outputs.output[_test_motor.motor_number] = _test_motor.value*2.0f-1.0f;
|
||||
_outputs.noutputs = _test_motor.motor_number+1;
|
||||
}
|
||||
new_output = true;
|
||||
} else if (controls_updated && (_mixers != nullptr)) {
|
||||
|
||||
// XXX one output group has 8 outputs max,
|
||||
@@ -358,39 +397,41 @@ int UavcanNode::run()
|
||||
unsigned num_outputs_max = 8;
|
||||
|
||||
// Do mixing
|
||||
outputs.noutputs = _mixers->mix(&outputs.output[0], num_outputs_max);
|
||||
outputs.timestamp = hrt_absolute_time();
|
||||
_outputs.noutputs = _mixers->mix(&_outputs.output[0], num_outputs_max);
|
||||
|
||||
// iterate actuators
|
||||
for (unsigned i = 0; i < outputs.noutputs; i++) {
|
||||
// last resort: catch NaN, INF and out-of-band errors
|
||||
if (!isfinite(outputs.output[i])) {
|
||||
/*
|
||||
* 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] = -1.0f;
|
||||
}
|
||||
|
||||
// limit outputs to valid range
|
||||
|
||||
// never go below min
|
||||
if (outputs.output[i] < -1.0f) {
|
||||
outputs.output[i] = -1.0f;
|
||||
}
|
||||
|
||||
// never go below max
|
||||
if (outputs.output[i] > 1.0f) {
|
||||
outputs.output[i] = 1.0f;
|
||||
}
|
||||
}
|
||||
|
||||
// Output to the bus
|
||||
_esc_controller.update_outputs(outputs.output, outputs.noutputs);
|
||||
new_output = true;
|
||||
}
|
||||
}
|
||||
|
||||
if (new_output) {
|
||||
// iterate actuators, checking for valid values
|
||||
for (uint8_t i = 0; i < _outputs.noutputs; i++) {
|
||||
// last resort: catch NaN, INF and out-of-band errors
|
||||
if (!isfinite(_outputs.output[i])) {
|
||||
/*
|
||||
* 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] = -1.0f;
|
||||
}
|
||||
|
||||
// never go below min
|
||||
if (_outputs.output[i] < -1.0f) {
|
||||
_outputs.output[i] = -1.0f;
|
||||
}
|
||||
|
||||
// never go above max
|
||||
if (_outputs.output[i] > 1.0f) {
|
||||
_outputs.output[i] = 1.0f;
|
||||
}
|
||||
}
|
||||
// Output to the bus
|
||||
_outputs.timestamp = hrt_absolute_time();
|
||||
_esc_controller.update_outputs(_outputs.output, _outputs.noutputs);
|
||||
}
|
||||
|
||||
|
||||
// Check motor test state
|
||||
bool updated = false;
|
||||
orb_check(_test_motor_sub, &updated);
|
||||
@@ -459,7 +500,6 @@ UavcanNode::subscribe()
|
||||
uint32_t sub_groups = _groups_required & ~_groups_subscribed;
|
||||
uint32_t unsub_groups = _groups_subscribed & ~_groups_required;
|
||||
// the first fd used by CAN
|
||||
_poll_fds_num = 1;
|
||||
for (unsigned i = 0; i < NUM_ACTUATOR_CONTROL_GROUPS; i++) {
|
||||
if (sub_groups & (1 << i)) {
|
||||
warnx("subscribe to actuator_controls_%d", i);
|
||||
@@ -472,9 +512,7 @@ UavcanNode::subscribe()
|
||||
}
|
||||
|
||||
if (_control_subs[i] > 0) {
|
||||
_poll_fds[_poll_fds_num].fd = _control_subs[i];
|
||||
_poll_fds[_poll_fds_num].events = POLLIN;
|
||||
_poll_fds_num++;
|
||||
_poll_ids[i] = add_poll_fd(_control_subs[i]);
|
||||
}
|
||||
}
|
||||
}
|
||||
@@ -572,6 +610,14 @@ UavcanNode::print_info()
|
||||
(unsigned)_groups_subscribed, (unsigned)_groups_required, _poll_fds_num);
|
||||
printf("ESC mixer: %s\n", (_mixers == nullptr) ? "NONE" : "OK");
|
||||
|
||||
if (_outputs.noutputs != 0) {
|
||||
printf("ESC output: ");
|
||||
for (uint8_t i=0; i<_outputs.noutputs; i++) {
|
||||
printf("%d ", (int)(_outputs.output[i]*1000));
|
||||
}
|
||||
printf("\n");
|
||||
}
|
||||
|
||||
// Sensor bridges
|
||||
auto br = _sensor_bridges.getHead();
|
||||
while (br != nullptr) {
|
||||
@@ -590,7 +636,7 @@ UavcanNode::print_info()
|
||||
static void print_usage()
|
||||
{
|
||||
warnx("usage: \n"
|
||||
"\tuavcan {start|status|stop}");
|
||||
"\tuavcan {start|status|stop|arm|disarm}");
|
||||
}
|
||||
|
||||
extern "C" __EXPORT int uavcan_main(int argc, char *argv[]);
|
||||
@@ -637,6 +683,16 @@ int uavcan_main(int argc, char *argv[])
|
||||
::exit(0);
|
||||
}
|
||||
|
||||
if (!std::strcmp(argv[1], "arm")) {
|
||||
inst->arm_actuators(true);
|
||||
::exit(0);
|
||||
}
|
||||
|
||||
if (!std::strcmp(argv[1], "disarm")) {
|
||||
inst->arm_actuators(false);
|
||||
::exit(0);
|
||||
}
|
||||
|
||||
if (!std::strcmp(argv[1], "stop")) {
|
||||
delete inst;
|
||||
::exit(0);
|
||||
|
||||
@@ -42,6 +42,7 @@
|
||||
#include <uORB/topics/actuator_outputs.h>
|
||||
#include <uORB/topics/actuator_armed.h>
|
||||
#include <uORB/topics/test_motor.h>
|
||||
#include <uORB/topics/actuator_direct.h>
|
||||
|
||||
#include "actuators/esc.hpp"
|
||||
#include "sensors/sensor_bridge.hpp"
|
||||
@@ -57,6 +58,9 @@
|
||||
#define NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN 4
|
||||
#define UAVCAN_DEVICE_PATH "/dev/uavcan/esc"
|
||||
|
||||
// we add two to allow for actuator_direct and busevent
|
||||
#define UAVCAN_NUM_POLL_FDS (NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN+2)
|
||||
|
||||
/**
|
||||
* A UAVCAN node.
|
||||
*/
|
||||
@@ -97,6 +101,8 @@ private:
|
||||
int init(uavcan::NodeID node_id);
|
||||
void node_spin_once();
|
||||
int run();
|
||||
int add_poll_fd(int fd); ///< add a fd to poll list, returning index into _poll_fds[]
|
||||
|
||||
|
||||
int _task = -1; ///< handle to the OS task
|
||||
bool _task_should_exit = false; ///< flag to indicate to tear down the CAN driver
|
||||
@@ -125,6 +131,15 @@ private:
|
||||
int _control_subs[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN] = {};
|
||||
actuator_controls_s _controls[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN] = {};
|
||||
orb_id_t _control_topics[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN] = {};
|
||||
pollfd _poll_fds[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN + 1] = {}; ///< +1 for /dev/uavcan/busevent
|
||||
pollfd _poll_fds[UAVCAN_NUM_POLL_FDS] = {};
|
||||
unsigned _poll_fds_num = 0;
|
||||
|
||||
int _actuator_direct_sub = -1; ///< uORB subscription of the actuator_direct topic
|
||||
uint8_t _actuator_direct_poll_fd_num;
|
||||
actuator_direct_s _actuator_direct;
|
||||
|
||||
actuator_outputs_s _outputs;
|
||||
|
||||
// index into _poll_fds for each _control_subs handle
|
||||
uint8_t _poll_ids[NUM_ACTUATOR_CONTROL_GROUPS_UAVCAN];
|
||||
};
|
||||
|
||||
Reference in New Issue
Block a user