forked from Archive/PX4-Autopilot
Send rc channel ordering and channel attributes from FMU to IO
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1b81724ef7
commit
0a89ab7075
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@ -72,6 +72,7 @@
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#include <systemlib/err.h>
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#include <systemlib/err.h>
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#include <systemlib/systemlib.h>
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#include <systemlib/systemlib.h>
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#include <systemlib/scheduling_priorities.h>
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#include <systemlib/scheduling_priorities.h>
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#include <systemlib/param/param.h>
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#include <uORB/topics/actuator_controls.h>
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#include <uORB/topics/actuator_controls.h>
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#include <uORB/topics/actuator_controls_effective.h>
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#include <uORB/topics/actuator_controls_effective.h>
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@ -608,6 +609,35 @@ PX4IO::io_send()
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/* set desired PWM output rate */
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/* set desired PWM output rate */
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cmd.servo_rate = _update_rate;
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cmd.servo_rate = _update_rate;
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/* maintaing the standard order of Roll, Pitch, Yaw, Throttle */
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cmd.rc_map[0] = param_find("RC_MAP_ROLL");
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cmd.rc_map[1] = param_find("RC_MAP_PITCH");
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cmd.rc_map[2] = param_find("RC_MAP_YAW");
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cmd.rc_map[3] = param_find("RC_MAP_THROTTLE");
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/* set the individual channel properties */
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char nbuf[16];
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for (unsigned i = 0; i < 4; i++) {
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sprintf(nbuf, "RC%d_MIN", i);
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cmd.rc_min[i] = (uint16_t)param_find(nbuf);
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}
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for (unsigned i = 0; i < 4; i++) {
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sprintf(nbuf, "RC%d_TRIM", i);
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cmd.rc_trim[i] = (uint16_t)param_find(nbuf);
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}
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for (unsigned i = 0; i < 4; i++) {
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sprintf(nbuf, "RC%d_MAX", i);
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cmd.rc_max[i] = (uint16_t)param_find(nbuf);
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}
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for (unsigned i = 0; i < 4; i++) {
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sprintf(nbuf, "RC%d_REV", i);
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cmd.rc_rev[i] = (uint16_t)param_find(nbuf);
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}
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for (unsigned i = 0; i < 4; i++) {
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sprintf(nbuf, "RC%d_DZ", i);
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cmd.rc_dz[i] = (uint16_t)param_find(nbuf);
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}
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ret = hx_stream_send(_io_stream, &cmd, sizeof(cmd));
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ret = hx_stream_send(_io_stream, &cmd, sizeof(cmd));
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if (ret)
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if (ret)
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@ -207,6 +207,19 @@ comms_handle_command(const void *buffer, size_t length)
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system_state.servo_rate = new_servo_rate;
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system_state.servo_rate = new_servo_rate;
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}
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}
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/* fetch the rc mappings */
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for (unsigned i = 0; i < 4; i++)
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system_state.rc_map[i] = cmd->rc_map[i];
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/* fetch the rc channel attributes */
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for (unsigned i = 0; i < 4; i++) {
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system_state.rc_min[i] = cmd->rc_min[i];
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system_state.rc_trim[i] = cmd->rc_trim[i];
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system_state.rc_max[i] = cmd->rc_max[i];
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system_state.rc_rev[i] = cmd->rc_rev[i];
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system_state.rc_dz[i] = cmd->rc_dz[i];
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}
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/*
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/*
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* update servo values immediately.
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* update servo values immediately.
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* the updates are done in addition also
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* the updates are done in addition also
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@ -67,6 +67,12 @@ extern "C" {
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*/
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*/
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#define FMU_INPUT_DROP_LIMIT_US 200000
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#define FMU_INPUT_DROP_LIMIT_US 200000
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/* XXX need to move the RC_CHANNEL_FUNCTION out of rc_channels.h and into systemlib */
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#define ROLL 0
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#define PITCH 1
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#define YAW 2
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#define THROTTLE 3
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/* current servo arm/disarm state */
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/* current servo arm/disarm state */
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bool mixer_servos_armed = false;
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bool mixer_servos_armed = false;
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@ -112,22 +118,22 @@ mixer_tick(void)
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/* when override is on or the fmu is not available, but RC is present */
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/* when override is on or the fmu is not available, but RC is present */
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control_count = system_state.rc_channels;
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control_count = system_state.rc_channels;
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// Remap the channels based on the radio type.
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// FMU: Roll, Pitch, Yaw, Throttle
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// Graupner: Throttle, Roll, Pitch, Yaw
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sched_lock();
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sched_lock();
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rc_channel_data[0] = system_state.rc_channel_data[1];
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rc_channel_data[1] = system_state.rc_channel_data[2];
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/* remap roll, pitch, yaw and throttle from RC specific to internal ordering */
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rc_channel_data[2] = system_state.rc_channel_data[3];
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rc_channel_data[ROLL] = system_state.rc_channel_data[system_state.rc_map[ROLL]];
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rc_channel_data[3] = system_state.rc_channel_data[0];
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rc_channel_data[PITCH] = system_state.rc_channel_data[system_state.rc_map[PITCH]];
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// AETR
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rc_channel_data[YAW] = system_state.rc_channel_data[system_state.rc_map[YAW]];
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//rc_channel_data[0] = system_state.rc_channel_data[0];
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rc_channel_data[THROTTLE] = system_state.rc_channel_data[system_state.rc_map[THROTTLE]];
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//rc_channel_data[1] = system_state.rc_channel_data[1];
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//rc_channel_data[2] = system_state.rc_channel_data[3];
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/* get the remaining channels, no remapping needed */
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//rc_channel_data[3] = system_state.rc_channel_data[2];
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for (unsigned i = 4; i < system_state.rc_channels; i++)
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for (unsigned i = 4; i < system_state.rc_channels; i++) {
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rc_channel_data[i] = system_state.rc_channel_data[i];
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rc_channel_data[i] = system_state.rc_channel_data[i];
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}
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/* scale the control inputs */
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rc_channel_data[THROTTLE] = ((rc_channel_data[THROTTLE] - system_state.rc_min[THROTTLE]) /
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(system_state.rc_max[THROTTLE] - system_state.rc_min[THROTTLE])) * 1000 + 1000;
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control_values = &rc_channel_data[0];
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control_values = &rc_channel_data[0];
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sched_unlock();
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sched_unlock();
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} else {
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} else {
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@ -60,6 +60,12 @@ struct px4io_command {
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bool arm_ok; /**< FMU allows full arming */
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bool arm_ok; /**< FMU allows full arming */
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bool vector_flight_mode_ok; /**< FMU aquired a valid position lock, ready for pos control */
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bool vector_flight_mode_ok; /**< FMU aquired a valid position lock, ready for pos control */
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bool manual_override_ok; /**< if true, IO performs a direct manual override */
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bool manual_override_ok; /**< if true, IO performs a direct manual override */
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uint16_t rc_map[4]; /**< channel ordering of roll, pitch, yaw, throttle */
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uint16_t rc_min[4]; /**< min value for each channel */
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uint16_t rc_trim[4]; /**< trim value for each channel */
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uint16_t rc_max[4]; /**< max value for each channel */
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uint16_t rc_rev[4]; /**< rev value for each channel */
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uint16_t rc_dz[4]; /**< dz value for each channel */
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};
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};
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/**
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/**
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@ -72,6 +72,20 @@ struct sys_state_s {
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bool arm_ok; /* FMU says OK to arm */
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bool arm_ok; /* FMU says OK to arm */
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uint16_t servo_rate; /* output rate of servos in Hz */
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uint16_t servo_rate; /* output rate of servos in Hz */
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/**
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* Remote control input(s) channel mappings
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*/
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uint16_t rc_map[4];
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/**
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* Remote control channel attributes
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*/
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uint16_t rc_min[4];
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uint16_t rc_trim[4];
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uint16_t rc_max[4];
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uint16_t rc_rev[4];
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uint16_t rc_dz[4];
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/**
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/**
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* Data from the remote control input(s)
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* Data from the remote control input(s)
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*/
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*/
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