forked from Archive/PX4-Autopilot
[WIP] simple simulation without sensor/estimator
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74303a79e1
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79538ac013
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@ -253,7 +253,7 @@ fi
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tone_alarm start
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rc_update start
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manual_control start
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sensors start
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#sensors start
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commander start
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if ! pwm_out_sim start -m sim
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@ -0,0 +1,5 @@
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CONFIG_EKF2_AUX_GLOBAL_POSITION=n
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CONFIG_EKF2_VERBOSE_STATUS=n
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CONFIG_MODULES_EKF2=n
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CONFIG_MODULES_SENSORS=y
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CONFIG_BOARD_NOLOCKSTEP=y
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@ -156,18 +156,18 @@ private:
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#ifndef CONSTRAINED_FLASH
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&_external_checks,
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#endif
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&_accelerometer_checks,
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&_airspeed_checks,
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//&_accelerometer_checks,
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//&_airspeed_checks,
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&_arm_permission_checks,
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&_baro_checks,
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//&_baro_checks,
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&_cpu_resource_checks,
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&_distance_sensor_checks,
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&_esc_checks,
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&_estimator_checks,
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&_failure_detector_checks,
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&_gyro_checks,
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&_imu_consistency_checks,
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&_magnetometer_checks,
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//&_gyro_checks,
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//&_imu_consistency_checks,
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//&_magnetometer_checks,
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&_manual_control_checks,
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&_home_position_checks,
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&_mission_checks,
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@ -531,6 +531,124 @@ void SimulatorMavlink::handle_message_hil_state_quaternion(const mavlink_message
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mavlink_hil_state_quaternion_t hil_state;
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mavlink_msg_hil_state_quaternion_decode(msg, &hil_state);
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uint64_t timestamp_sample = hrt_absolute_time(); // TODO: HIL_STATE_QUATERNION.time_us
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matrix::Quatf q(hil_state.attitude_quaternion);
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q.normalize();
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const matrix::Eulerf euler(q);
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// angular velocity
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{
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vehicle_angular_velocity_s angular_velocity{};
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angular_velocity.timestamp_sample = timestamp_sample;
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angular_velocity.xyz[0] = hil_state.rollspeed;
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angular_velocity.xyz[1] = hil_state.pitchspeed;
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angular_velocity.xyz[2] = hil_state.yawspeed;
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// TODO: add derivative fields
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// angular_velocity.xyz_derivative[0] = hil_state.rollspeed;
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// angular_velocity.xyz_derivative[1] = hil_state.pitchspeed;
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// angular_velocity.xyz_derivative[2] = hil_state.yawspeed;
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angular_velocity.timestamp = hrt_absolute_time();
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_vehicle_angular_velocity_pub.publish(angular_velocity);
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}
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// vehicle_acceleration // TODO:
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// vehicle_attitude
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{
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vehicle_attitude_s attitude{};
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attitude.timestamp_sample = timestamp_sample;
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q.copyTo(attitude.q);
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attitude.timestamp = hrt_absolute_time();
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_vehicle_attitude_pub.publish(attitude);
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}
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// vehicle_local_position
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{
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vehicle_local_position_s local_position{};
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local_position.timestamp_sample = timestamp_sample;
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double lat = hil_state.lat * 1e-7; // degE7 -> deg
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double lon = hil_state.lon * 1e-7; // degE7 -> deg
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if (!_global_local_proj_ref.isInitialized()) {
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_global_local_proj_ref.initReference(lat, lon);
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_global_local_alt0 = hil_state.alt / 1000.f; // mm -> m
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}
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local_position.xy_valid = true;
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local_position.z_valid = true;
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local_position.v_xy_valid = true;
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local_position.v_z_valid = true;
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_global_local_proj_ref.project(lat, lon, local_position.x, local_position.y);
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local_position.z = _global_local_alt0 - (hil_state.alt / 1000.f); // mm -> m
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local_position.vx = hil_state.vx / 100.f; // cm/s -> m/s
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local_position.vy = hil_state.vy / 100.f; // cm/s -> m/s
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local_position.vz = hil_state.vz / 100.f; // cm/s -> m/s
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local_position.z_deriv = local_position.vz;
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local_position.ax = hil_state.xacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
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local_position.ay = hil_state.yacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
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local_position.az = hil_state.zacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
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local_position.heading = euler.psi();
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local_position.unaided_heading = local_position.heading;
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local_position.xy_global = true;
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local_position.z_global = true;
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local_position.ref_timestamp = _global_local_proj_ref.getProjectionReferenceTimestamp();
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local_position.ref_lat = _global_local_proj_ref.getProjectionReferenceLat();
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local_position.ref_lon = _global_local_proj_ref.getProjectionReferenceLon();
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local_position.ref_alt = _global_local_alt0;
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local_position.dist_bottom = NAN;
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local_position.eph = 1.f;
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local_position.epv = 2.f;
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local_position.evh = 1.f;
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local_position.evv = 1.f;
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local_position.vxy_max = std::numeric_limits<float>::infinity();
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local_position.vz_max = std::numeric_limits<float>::infinity();
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local_position.hagl_min = std::numeric_limits<float>::infinity();
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local_position.hagl_max = std::numeric_limits<float>::infinity();
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local_position.timestamp = hrt_absolute_time();
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_vehicle_local_position_pub.publish(local_position);
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}
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// global position
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{
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vehicle_global_position_s global_position{};
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global_position.timestamp_sample = timestamp_sample;
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global_position.lat = hil_state.lat / 1e7;
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global_position.lon = hil_state.lon / 1e7;
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global_position.alt = hil_state.alt / 1e3;
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global_position.alt_ellipsoid = global_position.alt;
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global_position.eph = 1.f;
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global_position.epv = 2.f;
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global_position.terrain_alt = NAN;
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global_position.timestamp = hrt_absolute_time();
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_vehicle_global_position_pub.publish(global_position);
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}
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#if 0
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uint64_t timestamp = hrt_absolute_time();
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/* angular velocity */
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@ -614,6 +732,8 @@ void SimulatorMavlink::handle_message_hil_state_quaternion(const mavlink_message
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// always publish ground truth attitude message
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_lpos_ground_truth_pub.publish(hil_lpos);
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}
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#endif
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}
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void SimulatorMavlink::handle_message_landing_target(const mavlink_message_t *msg)
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@ -253,6 +253,15 @@ private:
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uORB::Publication<vehicle_local_position_s> _lpos_ground_truth_pub{ORB_ID(vehicle_local_position_groundtruth)};
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uORB::Publication<input_rc_s> _input_rc_pub{ORB_ID(input_rc)};
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uORB::Publication<vehicle_angular_velocity_s> _vehicle_angular_velocity_pub{ORB_ID(vehicle_angular_velocity)};
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uORB::Publication<vehicle_attitude_s> _vehicle_attitude_pub{ORB_ID(vehicle_attitude)};
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uORB::Publication<vehicle_global_position_s> _vehicle_global_position_pub{ORB_ID(vehicle_global_position)};
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uORB::Publication<vehicle_local_position_s> _vehicle_local_position_pub{ORB_ID(vehicle_local_position)};
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uORB::Publication<vehicle_odometry_s> _vehicle_odometry_pub{ORB_ID(vehicle_odometry)};
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//rpm
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uORB::Publication<rpm_s> _rpm_pub{ORB_ID(rpm)};
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