[WIP] simple simulation without sensor/estimator

This commit is contained in:
Daniel Agar 2024-02-15 14:57:37 -05:00
parent 74303a79e1
commit 79538ac013
5 changed files with 141 additions and 7 deletions

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@ -253,7 +253,7 @@ fi
tone_alarm start
rc_update start
manual_control start
sensors start
#sensors start
commander start
if ! pwm_out_sim start -m sim

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@ -0,0 +1,5 @@
CONFIG_EKF2_AUX_GLOBAL_POSITION=n
CONFIG_EKF2_VERBOSE_STATUS=n
CONFIG_MODULES_EKF2=n
CONFIG_MODULES_SENSORS=y
CONFIG_BOARD_NOLOCKSTEP=y

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@ -156,18 +156,18 @@ private:
#ifndef CONSTRAINED_FLASH
&_external_checks,
#endif
&_accelerometer_checks,
&_airspeed_checks,
//&_accelerometer_checks,
//&_airspeed_checks,
&_arm_permission_checks,
&_baro_checks,
//&_baro_checks,
&_cpu_resource_checks,
&_distance_sensor_checks,
&_esc_checks,
&_estimator_checks,
&_failure_detector_checks,
&_gyro_checks,
&_imu_consistency_checks,
&_magnetometer_checks,
//&_gyro_checks,
//&_imu_consistency_checks,
//&_magnetometer_checks,
&_manual_control_checks,
&_home_position_checks,
&_mission_checks,

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@ -531,6 +531,124 @@ void SimulatorMavlink::handle_message_hil_state_quaternion(const mavlink_message
mavlink_hil_state_quaternion_t hil_state;
mavlink_msg_hil_state_quaternion_decode(msg, &hil_state);
uint64_t timestamp_sample = hrt_absolute_time(); // TODO: HIL_STATE_QUATERNION.time_us
matrix::Quatf q(hil_state.attitude_quaternion);
q.normalize();
const matrix::Eulerf euler(q);
// angular velocity
{
vehicle_angular_velocity_s angular_velocity{};
angular_velocity.timestamp_sample = timestamp_sample;
angular_velocity.xyz[0] = hil_state.rollspeed;
angular_velocity.xyz[1] = hil_state.pitchspeed;
angular_velocity.xyz[2] = hil_state.yawspeed;
// TODO: add derivative fields
// angular_velocity.xyz_derivative[0] = hil_state.rollspeed;
// angular_velocity.xyz_derivative[1] = hil_state.pitchspeed;
// angular_velocity.xyz_derivative[2] = hil_state.yawspeed;
angular_velocity.timestamp = hrt_absolute_time();
_vehicle_angular_velocity_pub.publish(angular_velocity);
}
// vehicle_acceleration // TODO:
// vehicle_attitude
{
vehicle_attitude_s attitude{};
attitude.timestamp_sample = timestamp_sample;
q.copyTo(attitude.q);
attitude.timestamp = hrt_absolute_time();
_vehicle_attitude_pub.publish(attitude);
}
// vehicle_local_position
{
vehicle_local_position_s local_position{};
local_position.timestamp_sample = timestamp_sample;
double lat = hil_state.lat * 1e-7; // degE7 -> deg
double lon = hil_state.lon * 1e-7; // degE7 -> deg
if (!_global_local_proj_ref.isInitialized()) {
_global_local_proj_ref.initReference(lat, lon);
_global_local_alt0 = hil_state.alt / 1000.f; // mm -> m
}
local_position.xy_valid = true;
local_position.z_valid = true;
local_position.v_xy_valid = true;
local_position.v_z_valid = true;
_global_local_proj_ref.project(lat, lon, local_position.x, local_position.y);
local_position.z = _global_local_alt0 - (hil_state.alt / 1000.f); // mm -> m
local_position.vx = hil_state.vx / 100.f; // cm/s -> m/s
local_position.vy = hil_state.vy / 100.f; // cm/s -> m/s
local_position.vz = hil_state.vz / 100.f; // cm/s -> m/s
local_position.z_deriv = local_position.vz;
local_position.ax = hil_state.xacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
local_position.ay = hil_state.yacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
local_position.az = hil_state.zacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
local_position.heading = euler.psi();
local_position.unaided_heading = local_position.heading;
local_position.xy_global = true;
local_position.z_global = true;
local_position.ref_timestamp = _global_local_proj_ref.getProjectionReferenceTimestamp();
local_position.ref_lat = _global_local_proj_ref.getProjectionReferenceLat();
local_position.ref_lon = _global_local_proj_ref.getProjectionReferenceLon();
local_position.ref_alt = _global_local_alt0;
local_position.dist_bottom = NAN;
local_position.eph = 1.f;
local_position.epv = 2.f;
local_position.evh = 1.f;
local_position.evv = 1.f;
local_position.vxy_max = std::numeric_limits<float>::infinity();
local_position.vz_max = std::numeric_limits<float>::infinity();
local_position.hagl_min = std::numeric_limits<float>::infinity();
local_position.hagl_max = std::numeric_limits<float>::infinity();
local_position.timestamp = hrt_absolute_time();
_vehicle_local_position_pub.publish(local_position);
}
// global position
{
vehicle_global_position_s global_position{};
global_position.timestamp_sample = timestamp_sample;
global_position.lat = hil_state.lat / 1e7;
global_position.lon = hil_state.lon / 1e7;
global_position.alt = hil_state.alt / 1e3;
global_position.alt_ellipsoid = global_position.alt;
global_position.eph = 1.f;
global_position.epv = 2.f;
global_position.terrain_alt = NAN;
global_position.timestamp = hrt_absolute_time();
_vehicle_global_position_pub.publish(global_position);
}
#if 0
uint64_t timestamp = hrt_absolute_time();
/* angular velocity */
@ -614,6 +732,8 @@ void SimulatorMavlink::handle_message_hil_state_quaternion(const mavlink_message
// always publish ground truth attitude message
_lpos_ground_truth_pub.publish(hil_lpos);
}
#endif
}
void SimulatorMavlink::handle_message_landing_target(const mavlink_message_t *msg)

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@ -253,6 +253,15 @@ private:
uORB::Publication<vehicle_local_position_s> _lpos_ground_truth_pub{ORB_ID(vehicle_local_position_groundtruth)};
uORB::Publication<input_rc_s> _input_rc_pub{ORB_ID(input_rc)};
uORB::Publication<vehicle_angular_velocity_s> _vehicle_angular_velocity_pub{ORB_ID(vehicle_angular_velocity)};
uORB::Publication<vehicle_attitude_s> _vehicle_attitude_pub{ORB_ID(vehicle_attitude)};
uORB::Publication<vehicle_global_position_s> _vehicle_global_position_pub{ORB_ID(vehicle_global_position)};
uORB::Publication<vehicle_local_position_s> _vehicle_local_position_pub{ORB_ID(vehicle_local_position)};
uORB::Publication<vehicle_odometry_s> _vehicle_odometry_pub{ORB_ID(vehicle_odometry)};
//rpm
uORB::Publication<rpm_s> _rpm_pub{ORB_ID(rpm)};