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EKF: fix code style
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+74
-70
@@ -43,87 +43,91 @@
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void Ekf::controlFusionModes()
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{
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// Determine the vehicle status
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calculateVehicleStatus();
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// Determine the vehicle status
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calculateVehicleStatus();
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// optical flow fusion mode selection logic
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_control_status.flags.opt_flow = false;
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// optical flow fusion mode selection logic
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_control_status.flags.opt_flow = false;
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// GPS fusion mode selection logic
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// To start use GPS we need angular alignment completed, the local NED origin set and fresh GPS data
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if (!_control_status.flags.gps) {
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if (_control_status.flags.angle_align && (_time_last_imu - _time_last_gps) < 5e5 && _NED_origin_initialised && (_time_last_imu - _last_gps_fail_us > 5e6)) {
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_control_status.flags.gps = true;
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resetPosition();
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resetVelocity();
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}
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}
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// GPS fusion mode selection logic
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// To start use GPS we need angular alignment completed, the local NED origin set and fresh GPS data
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if (!_control_status.flags.gps) {
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if (_control_status.flags.angle_align && (_time_last_imu - _time_last_gps) < 5e5 && _NED_origin_initialised
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&& (_time_last_imu - _last_gps_fail_us > 5e6)) {
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_control_status.flags.gps = true;
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resetPosition();
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resetVelocity();
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}
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}
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// decide when to start using optical flow data
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if (!_control_status.flags.opt_flow) {
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// TODO optical flow start logic
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}
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// decide when to start using optical flow data
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if (!_control_status.flags.opt_flow) {
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// TODO optical flow start logic
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}
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// handle the case when we are relying on GPS fusion and lose it
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if (_control_status.flags.gps && !_control_status.flags.opt_flow) {
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// We are relying on GPS aiding to constrain attitude drift so after 10 seconds without aiding we need to do something
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if ((_time_last_imu - _time_last_pos_fuse > 10e6) && (_time_last_imu - _time_last_vel_fuse > 10e6)) {
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if (_time_last_imu - _time_last_gps > 5e5) {
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// if we don't have gps then we need to switch to the non-aiding mode, zero the veloity states
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// and set the synthetic GPS position to the current estimate
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_control_status.flags.gps = false;
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_last_known_posNE(0) = _state.pos(0);
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_last_known_posNE(1) = _state.pos(1);
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_state.vel.setZero();
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} else {
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// Reset states to the last GPS measurement
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resetPosition();
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resetVelocity();
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}
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}
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}
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// handle the case when we are relying on GPS fusion and lose it
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if (_control_status.flags.gps && !_control_status.flags.opt_flow) {
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// We are relying on GPS aiding to constrain attitude drift so after 10 seconds without aiding we need to do something
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if ((_time_last_imu - _time_last_pos_fuse > 10e6) && (_time_last_imu - _time_last_vel_fuse > 10e6)) {
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if (_time_last_imu - _time_last_gps > 5e5) {
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// if we don't have gps then we need to switch to the non-aiding mode, zero the veloity states
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// and set the synthetic GPS position to the current estimate
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_control_status.flags.gps = false;
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_last_known_posNE(0) = _state.pos(0);
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_last_known_posNE(1) = _state.pos(1);
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_state.vel.setZero();
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// handle the case when we are relying on optical flow fusion and lose it
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if (_control_status.flags.opt_flow && !_control_status.flags.gps) {
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// TODO
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}
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} else {
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// Reset states to the last GPS measurement
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resetPosition();
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resetVelocity();
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}
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}
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}
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// Determine if we should use simple magnetic heading fusion which works better when there are large external disturbances
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// or the more accurate 3-axis fusion
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if (!_control_status.flags.armed) {
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// always use simple mag fusion for initial startup
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_control_status.flags.mag_hdg = true;
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_control_status.flags.mag_3D = false;
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} else {
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if (_control_status.flags.in_air) {
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// always use 3-axis mag fusion when airborne
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_control_status.flags.mag_hdg = false;
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_control_status.flags.mag_3D = true;
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} else {
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// always use simple heading fusion when on the ground
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_control_status.flags.mag_hdg = true;
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_control_status.flags.mag_3D = false;
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}
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}
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// handle the case when we are relying on optical flow fusion and lose it
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if (_control_status.flags.opt_flow && !_control_status.flags.gps) {
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// TODO
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}
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// Determine if we should use simple magnetic heading fusion which works better when there are large external disturbances
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// or the more accurate 3-axis fusion
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if (!_control_status.flags.armed) {
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// always use simple mag fusion for initial startup
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_control_status.flags.mag_hdg = true;
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_control_status.flags.mag_3D = false;
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} else {
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if (_control_status.flags.in_air) {
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// always use 3-axis mag fusion when airborne
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_control_status.flags.mag_hdg = false;
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_control_status.flags.mag_3D = true;
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} else {
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// always use simple heading fusion when on the ground
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_control_status.flags.mag_hdg = true;
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_control_status.flags.mag_3D = false;
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}
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}
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}
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void Ekf::calculateVehicleStatus()
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{
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// determine if the vehicle is armed
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_control_status.flags.armed = _vehicle_armed;
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// determine if the vehicle is armed
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_control_status.flags.armed = _vehicle_armed;
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// record vertical position whilst disarmed to use as a height change reference
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if (!_control_status.flags.armed) {
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_last_disarmed_posD = _state.pos(2);
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}
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// record vertical position whilst disarmed to use as a height change reference
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if (!_control_status.flags.armed) {
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_last_disarmed_posD = _state.pos(2);
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}
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// Transition to in-air occurs when armed and when altitude has increased sufficiently from the altitude at arming
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if (!_control_status.flags.in_air && _control_status.flags.armed && (_state.pos(2) - _last_disarmed_posD) < -1.0f) {
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_control_status.flags.in_air = true;
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}
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// Transition to in-air occurs when armed and when altitude has increased sufficiently from the altitude at arming
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if (!_control_status.flags.in_air && _control_status.flags.armed && (_state.pos(2) - _last_disarmed_posD) < -1.0f) {
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_control_status.flags.in_air = true;
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}
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// Transition to on-ground occurs when disarmed.
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if (_control_status.flags.in_air && !_control_status.flags.armed) {
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_control_status.flags.in_air = false;
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}
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// Transition to on-ground occurs when disarmed.
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if (_control_status.flags.in_air && !_control_status.flags.armed) {
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_control_status.flags.in_air = false;
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}
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}
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