From c51ec3411850d9de0794d4e584838d4a137dafcf Mon Sep 17 00:00:00 2001 From: Roman Bapst Date: Wed, 5 Nov 2014 08:50:20 +0100 Subject: added initialisation of parameters, added assignment of actuator controls, cleaned up --- src/modules/mc_att_control/mc_att_control_base.cpp | 53 ++++++++++++++++++---- 1 file changed, 45 insertions(+), 8 deletions(-) diff --git a/src/modules/mc_att_control/mc_att_control_base.cpp b/src/modules/mc_att_control/mc_att_control_base.cpp index d39bae4dc..fee117458 100644 --- a/src/modules/mc_att_control/mc_att_control_base.cpp +++ b/src/modules/mc_att_control/mc_att_control_base.cpp @@ -51,6 +51,27 @@ MulticopterAttitudeControlBase::MulticopterAttitudeControlBase() : _att_control.zero(); _I.identity(); + + // setup standard gains + _params.att_p(0) = 5.0; + _params.rate_p(0) = 0.05; + _params.rate_i(0) = 0.0; + _params.rate_d(0) = 0.003; + /* pitch gains */ + _params.att_p(1) = 5.0; + _params.rate_p(1) = 0.05; + _params.rate_i(1) = 0.0; + _params.rate_d(1) = 0.003; + /* yaw gains */ + _params.att_p(2) = 2.8; + _params.rate_p(2) = 0.2; + _params.rate_i(2) = 0.1; + _params.rate_d(2) = 0.0; + _params.yaw_rate_max = 0.5; + _params.yaw_ff = 0.5; + _params.man_roll_max = 0.6; + _params.man_pitch_max = 0.6; + _params.man_yaw_max = 0.6; } MulticopterAttitudeControlBase::~MulticopterAttitudeControlBase() { @@ -282,13 +303,21 @@ void MulticopterAttitudeControlBase::control_attitude_rates(float dt) { } -void MulticopterAttitudeControlBase::set_attitude(const Eigen::Quaternion& attitude) { +void MulticopterAttitudeControlBase::set_actuator_controls() { + _actuators.control[0] = (isfinite(_att_control(0))) ? _att_control(0) : 0.0f; + _actuators.control[1] = (isfinite(_att_control(1))) ? _att_control(1) : 0.0f; + _actuators.control[2] = (isfinite(_att_control(2))) ? _att_control(2) : 0.0f; + _actuators.control[3] = (isfinite(_thrust_sp)) ? _thrust_sp : 0.0f; + //_actuators.timestamp = hrt_absolute_time(); +} + +void MulticopterAttitudeControlBase::set_attitude(const Eigen::Quaternion attitude) { // check if this is consistent !!! - math::Vector<3> quat; - quat(0) = attitude(0); - quat(1) = attitude(1); - quat(2) = attitude(2); - quat(3) = attitude(3); + math::Quaternion quat; + quat(0) = (float)attitude.w(); + quat(1) = (float)attitude.x(); + quat(2) = (float)attitude.y(); + quat(3) = (float)attitude.z(); _v_att.q[0] = quat(0); _v_att.q[1] = quat(1); @@ -322,11 +351,11 @@ void MulticopterAttitudeControlBase::set_attitude_reference(const Eigen::Vector4 _v_att_sp.roll_body = control_attitude_thrust_reference(0); _v_att_sp.pitch_body = control_attitude_thrust_reference(1); _v_att_sp.yaw_body = control_attitude_thrust_reference(2); - _v_att_sp.thrust = control_attitude_thrust_reference(3); + _v_att_sp.thrust = (control_attitude_thrust_referenc(3) -30)*(-1)/30; // setup rotation matrix math::Matrix<3,3> Rot_sp; - Rot_sp = R.from_euler(_v_att_sp.roll_body,_v_att_sp.pitch_body,_v_att_sp.yaw_body); + Rot_sp.from_euler(_v_att_sp.roll_body,_v_att_sp.pitch_body,_v_att_sp.yaw_body); _v_att_sp.R_body[0][0] = Rot_sp(0,0); _v_att_sp.R_body[1][0] = Rot_sp(1,0); _v_att_sp.R_body[2][0] = Rot_sp(2,0); @@ -338,3 +367,11 @@ void MulticopterAttitudeControlBase::set_attitude_reference(const Eigen::Vector4 _v_att_sp.R_body[2][2] = Rot_sp(2,2); } + +void MulticopterAttitudeControlBase::get_mixer_input(Eigen::Vector4d& motor_inputs) { + motor_inputs(0) = _actuators.control[0]; + motor_inputs(1) = _actuators.control[1]; + motor_inputs(2) = _actuators.control[2]; + motor_inputs(3) = _actuators.control[3]; +} + -- cgit v1.2.3