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synced 2026-10-23 09:33:34 +08:00
gimbal: Add test command for angle rates
This is handy to test angular rate input, not just angles.
This commit is contained in:
@@ -1,6 +1,6 @@
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/****************************************************************************
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/****************************************************************************
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*
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*
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* Copyright (c) 2013-2023 PX4 Development Team. All rights reserved.
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* Copyright (c) 2013-2024 PX4 Development Team. All rights reserved.
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*
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*
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* Redistribution and use in source and binary forms, with or without
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* modification, are permitted provided that the following conditions
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@@ -369,27 +369,77 @@ int gimbal_main(int argc, char *argv[])
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if (thread_running.load() && g_thread_data && g_thread_data->test_input) {
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if (thread_running.load() && g_thread_data && g_thread_data->test_input) {
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if (argc >= 4) {
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if (argc >= 4) {
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bool found_axis = false;
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const char *axis_names[3] = {"roll", "pitch", "yaw"};
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float roll_deg = 0.0f;
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int angles[3] = { 0, 0, 0 };
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float pitch_deg = 0.0f;
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float yaw_deg = 0.0f;
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float rollrate_deg_s = 0.0f;
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float pitchrate_deg_s = 0.0f;
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float yawrate_deg_s = 0.0f;
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bool angles_set = false;
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bool rates_set = false;
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for (int arg_i = 2 ; arg_i < (argc - 1); ++arg_i) {
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for (int arg_i = 2 ; arg_i < (argc - 1); ++arg_i) {
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for (int axis_i = 0; axis_i < 3; ++axis_i) {
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if (!strcmp(argv[arg_i], axis_names[axis_i])) {
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if (!strcmp(argv[arg_i], "roll")) {
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int angle_deg = (int)strtol(argv[arg_i + 1], nullptr, 0);
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roll_deg = (int)strtof(argv[arg_i + 1], nullptr);
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angles[axis_i] = angle_deg;
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angles_set = true;
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found_axis = true;
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}
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} else if (!strcmp(argv[arg_i], "pitch")) {
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pitch_deg = (int)strtof(argv[arg_i + 1], nullptr);
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angles_set = true;
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} else if (!strcmp(argv[arg_i], "yaw")) {
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yaw_deg = (int)strtof(argv[arg_i + 1], nullptr);
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angles_set = true;
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} else if (!strcmp(argv[arg_i], "rollrate")) {
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rollrate_deg_s = (int)strtof(argv[arg_i + 1], nullptr);
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rates_set = true;
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} else if (!strcmp(argv[arg_i], "pitchrate")) {
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pitchrate_deg_s = (int)strtof(argv[arg_i + 1], nullptr);
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rates_set = true;
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} else if (!strcmp(argv[arg_i], "yawrate")) {
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yawrate_deg_s = (int)strtof(argv[arg_i + 1], nullptr);
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rates_set = true;
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} else {
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PX4_ERR("Unknown argument: %s", argv[arg_i]);
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usage();
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return -1;
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}
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}
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}
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}
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if (!found_axis) {
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if (angles_set && rates_set) {
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PX4_ERR("This driver doesn't support both, angles and rates, to be set");
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usage();
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return -1;
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} else if (angles_set) {
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g_thread_data->test_input->set_test_input_angles(
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roll_deg,
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pitch_deg,
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yaw_deg
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);
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return 0;
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} else if (rates_set) {
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g_thread_data->test_input->set_test_input_angle_rates(
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rollrate_deg_s,
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pitchrate_deg_s,
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yawrate_deg_s
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);
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return 0;
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} else {
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PX4_ERR("No angles or angle rates set");
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usage();
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usage();
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return -1;
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return -1;
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}
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}
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g_thread_data->test_input->set_test_input(angles[0], angles[1], angles[2]);
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return 0;
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}
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}
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} else {
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} else {
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@@ -573,5 +623,6 @@ $ gimbal test pitch -45 yaw 30
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PRINT_MODULE_USAGE_ARG("<sysid> <compid>", "MAVLink system ID and MAVLink component ID", false);
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PRINT_MODULE_USAGE_ARG("<sysid> <compid>", "MAVLink system ID and MAVLink component ID", false);
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PRINT_MODULE_USAGE_COMMAND_DESCR("test", "Test the output: set a fixed angle for one or multiple axes (gimbal must be running)");
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PRINT_MODULE_USAGE_COMMAND_DESCR("test", "Test the output: set a fixed angle for one or multiple axes (gimbal must be running)");
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PRINT_MODULE_USAGE_ARG("roll|pitch|yaw <angle>", "Specify an axis and an angle in degrees", false);
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PRINT_MODULE_USAGE_ARG("roll|pitch|yaw <angle>", "Specify an axis and an angle in degrees", false);
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PRINT_MODULE_USAGE_ARG("rollrate|pitchrate|yawrate <angle rate>", "Specify an axis and an angle rate in degrees / second", false);
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PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
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PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
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}
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}
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@@ -55,21 +55,30 @@ InputTest::UpdateResult InputTest::update(unsigned int timeout_ms, ControlData &
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control_data.type = ControlData::Type::Angle;
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control_data.type = ControlData::Type::Angle;
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control_data.timestamp_last_update = hrt_absolute_time();
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control_data.timestamp_last_update = hrt_absolute_time();
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control_data.type_data.angle.frames[0] = ControlData::TypeData::TypeAngle::Frame::AngleAbsoluteFrame;
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if (PX4_ISFINITE(_roll_deg) && PX4_ISFINITE(_pitch_deg) && PX4_ISFINITE(_yaw_deg)) {
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control_data.type_data.angle.frames[1] = ControlData::TypeData::TypeAngle::Frame::AngleAbsoluteFrame;
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control_data.type_data.angle.frames[0] = ControlData::TypeData::TypeAngle::Frame::AngleAbsoluteFrame;
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control_data.type_data.angle.frames[2] = ControlData::TypeData::TypeAngle::Frame::AngleBodyFrame;
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control_data.type_data.angle.frames[1] = ControlData::TypeData::TypeAngle::Frame::AngleAbsoluteFrame;
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control_data.type_data.angle.frames[2] = ControlData::TypeData::TypeAngle::Frame::AngleBodyFrame;
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matrix::Eulerf euler(
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math::radians((float)_roll_deg),
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math::radians((float)_pitch_deg),
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math::radians((float)_yaw_deg));
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matrix::Quatf q(euler);
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q.copyTo(control_data.type_data.angle.q);
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matrix::Eulerf euler(
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} else {
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math::radians((float)_roll_deg),
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control_data.type_data.angle.frames[0] = ControlData::TypeData::TypeAngle::Frame::AngularRate;
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math::radians((float)_pitch_deg),
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control_data.type_data.angle.frames[1] = ControlData::TypeData::TypeAngle::Frame::AngularRate;
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math::radians((float)_yaw_deg));
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control_data.type_data.angle.frames[2] = ControlData::TypeData::TypeAngle::Frame::AngularRate;
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matrix::Quatf q(euler);
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control_data.type_data.angle.q[0] = NAN;
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control_data.type_data.angle.q[1] = NAN;
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control_data.type_data.angle.q[2] = NAN;
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control_data.type_data.angle.q[3] = NAN;
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control_data.type_data.angle.angular_velocity[0] = math::radians(_rollrate_deg_s);
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control_data.type_data.angle.angular_velocity[1] = math::radians(_pitchrate_deg_s);
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control_data.type_data.angle.angular_velocity[2] = math::radians(_yawrate_deg_s);
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}
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q.copyTo(control_data.type_data.angle.q);
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control_data.type_data.angle.angular_velocity[0] = NAN;
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control_data.type_data.angle.angular_velocity[1] = NAN;
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control_data.type_data.angle.angular_velocity[2] = NAN;
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// For testing we mark ourselves as in control.
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// For testing we mark ourselves as in control.
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control_data.sysid_primary_control = _parameters.mav_sysid;
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control_data.sysid_primary_control = _parameters.mav_sysid;
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@@ -87,17 +96,32 @@ int InputTest::initialize()
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void InputTest::print_status() const
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void InputTest::print_status() const
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{
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{
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PX4_INFO("Input: Test");
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PX4_INFO("Input: Test");
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PX4_INFO_RAW(" roll : % 3d deg\n", _roll_deg);
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PX4_INFO_RAW(" roll : % .1f deg\n", (double)_roll_deg);
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PX4_INFO_RAW(" pitch: % 3d deg\n", _pitch_deg);
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PX4_INFO_RAW(" pitch: % .1f deg\n", (double)_pitch_deg);
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PX4_INFO_RAW(" yaw : % 3d deg\n", _yaw_deg);
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PX4_INFO_RAW(" yaw : % .1f deg\n", (double)_yaw_deg);
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PX4_INFO_RAW(" rollrate : % .1f deg/s\n", (double)_rollrate_deg_s);
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PX4_INFO_RAW(" pitchrate: % .1f deg/s\n", (double)_pitchrate_deg_s);
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PX4_INFO_RAW(" yawrate : % .1f deg/s\n", (double)_yawrate_deg_s);
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}
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}
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void InputTest::set_test_input(int roll_deg, int pitch_deg, int yaw_deg)
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void InputTest::set_test_input_angles(float roll_deg, float pitch_deg, float yaw_deg)
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{
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{
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_roll_deg = roll_deg;
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_roll_deg = roll_deg;
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_pitch_deg = pitch_deg;
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_pitch_deg = pitch_deg;
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_yaw_deg = yaw_deg;
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_yaw_deg = yaw_deg;
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_rollrate_deg_s = NAN;
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_pitchrate_deg_s = NAN;
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_yawrate_deg_s = NAN;
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_has_been_set.store(true);
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}
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void InputTest::set_test_input_angle_rates(float rollrate_deg_s, float pitchrate_deg_s, float yawrate_deg_s)
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{
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_roll_deg = NAN;
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_pitch_deg = NAN;
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_yaw_deg = NAN;
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_rollrate_deg_s = rollrate_deg_s;
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_pitchrate_deg_s = pitchrate_deg_s;
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_yawrate_deg_s = yawrate_deg_s;
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_has_been_set.store(true);
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_has_been_set.store(true);
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}
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}
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@@ -50,12 +50,17 @@ public:
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int initialize() override;
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int initialize() override;
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void print_status() const override;
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void print_status() const override;
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void set_test_input(int roll_deg, int pitch_deg, int yaw_deg);
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void set_test_input_angles(
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float roll_deg, float pitch_deg, float yaw_deg);
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void set_test_input_angle_rates(float rollrate_deg_s, float pitchrate_deg_s, float yawrate_deg_s);
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private:
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private:
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int _roll_deg {0};
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float _roll_deg {NAN};
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int _pitch_deg {0};
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float _pitch_deg {NAN};
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int _yaw_deg {0};
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float _yaw_deg {NAN};
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float _rollrate_deg_s {NAN};
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float _pitchrate_deg_s {NAN};
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float _yawrate_deg_s {NAN};
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px4::atomic<bool> _has_been_set {false};
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px4::atomic<bool> _has_been_set {false};
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};
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};
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