mirror of https://github.com/ArduPilot/ardupilot
Plane: Add VTOL descent rate, convert existing rate to climb rate only
Co-authored-by: Reko Merio K9260@student.jamk.fi Co-authored-by: Peter Barker <pb-gh@barker.dropbear.id.au>
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@ -41,7 +41,7 @@ void QAutoTune::get_pilot_desired_rp_yrate_cd(float &des_roll_cd, float &des_pit
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void QAutoTune::init_z_limits()
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{
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plane.quadplane.pos_control->set_max_speed_z(-plane.quadplane.pilot_velocity_z_max, plane.quadplane.pilot_velocity_z_max);
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plane.quadplane.pos_control->set_max_speed_z(-plane.quadplane.get_pilot_velocity_z_max_dn(), plane.quadplane.pilot_velocity_z_max_up);
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plane.quadplane.pos_control->set_max_accel_z(plane.quadplane.pilot_accel_z);
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}
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@ -39,13 +39,22 @@ const AP_Param::GroupInfo QuadPlane::var_info[] = {
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AP_SUBGROUPPTR(pos_control, "P", 17, QuadPlane, AC_PosControl),
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// @Param: VELZ_MAX
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// @DisplayName: Pilot maximum vertical speed
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// @Description: The maximum vertical velocity the pilot may request in cm/s
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// @DisplayName: Pilot maximum vertical speed up
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// @Description: The maximum ascending vertical velocity the pilot may request in cm/s
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// @Units: cm/s
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// @Range: 50 500
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// @Increment: 10
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// @User: Standard
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AP_GROUPINFO("VELZ_MAX", 18, QuadPlane, pilot_velocity_z_max, 250),
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AP_GROUPINFO("VELZ_MAX", 18, QuadPlane, pilot_velocity_z_max_up, 250),
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// @Param: VELZ_MAX_DN
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// @DisplayName: Pilot maximum vertical speed down
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// @Description: The maximum vertical velocity the pilot may request in cm/s going down. If 0, uses Q_VELZ_MAX value.
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// @Units: cm/s
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// @Range: 50 500
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// @Increment: 10
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// @User: Standard
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AP_GROUPINFO("VELZ_MAX_DN", 60, QuadPlane, pilot_velocity_z_max_dn, 0),
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// @Param: ACCEL_Z
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// @DisplayName: Pilot vertical acceleration
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@ -335,6 +344,8 @@ const AP_Param::GroupInfo QuadPlane::var_info[] = {
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AP_SUBGROUPEXTENSION("",59, QuadPlane, var_info2),
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// 60 is used above for VELZ_MAX_DN
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AP_GROUPEND
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};
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@ -1059,7 +1070,7 @@ void QuadPlane::run_z_controller(void)
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pos_control->set_desired_velocity_z(inertial_nav.get_velocity_z());
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// initialize vertical speeds and leash lengths
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pos_control->set_max_speed_z(-pilot_velocity_z_max, pilot_velocity_z_max);
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pos_control->set_max_speed_z(-get_pilot_velocity_z_max_dn(), pilot_velocity_z_max_up);
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pos_control->set_max_accel_z(pilot_accel_z);
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// it has been two seconds since we last ran the Z
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@ -1112,7 +1123,7 @@ void QuadPlane::init_qacro(void)
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void QuadPlane::init_hover(void)
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{
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// initialize vertical speeds and leash lengths
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pos_control->set_max_speed_z(-pilot_velocity_z_max, pilot_velocity_z_max);
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pos_control->set_max_speed_z(-get_pilot_velocity_z_max_dn(), pilot_velocity_z_max_up);
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pos_control->set_max_accel_z(pilot_accel_z);
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// initialise position and desired velocity
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@ -1148,7 +1159,7 @@ void QuadPlane::hold_hover(float target_climb_rate)
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motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
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// initialize vertical speeds and acceleration
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pos_control->set_max_speed_z(-pilot_velocity_z_max, pilot_velocity_z_max);
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pos_control->set_max_speed_z(-get_pilot_velocity_z_max_dn(), pilot_velocity_z_max_up);
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pos_control->set_max_accel_z(pilot_accel_z);
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// call attitude controller
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@ -1279,7 +1290,7 @@ void QuadPlane::init_loiter(void)
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loiter_nav->init_target();
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// initialize vertical speed and acceleration
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pos_control->set_max_speed_z(-pilot_velocity_z_max, pilot_velocity_z_max);
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pos_control->set_max_speed_z(-get_pilot_velocity_z_max_dn(), pilot_velocity_z_max_up);
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pos_control->set_max_accel_z(pilot_accel_z);
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// initialise position and desired velocity
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@ -1426,7 +1437,7 @@ void QuadPlane::control_loiter()
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motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
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// initialize vertical speed and acceleration
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pos_control->set_max_speed_z(-pilot_velocity_z_max, pilot_velocity_z_max);
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pos_control->set_max_speed_z(-get_pilot_velocity_z_max_dn(), pilot_velocity_z_max_up);
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pos_control->set_max_accel_z(pilot_accel_z);
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// process pilot's roll and pitch input
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@ -1542,7 +1553,8 @@ float QuadPlane::get_pilot_desired_climb_rate_cms(void) const
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}
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uint16_t dead_zone = plane.channel_throttle->get_dead_zone();
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uint16_t trim = (plane.channel_throttle->get_radio_max() + plane.channel_throttle->get_radio_min())/2;
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return pilot_velocity_z_max * plane.channel_throttle->pwm_to_angle_dz_trim(dead_zone, trim) / 100.0f;
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const float throttle_request = plane.channel_throttle->pwm_to_angle_dz_trim(dead_zone, trim) *0.01f;
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return throttle_request * (throttle_request > 0.0f ? pilot_velocity_z_max_up : get_pilot_velocity_z_max_dn());
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}
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@ -2665,7 +2677,7 @@ void QuadPlane::setup_target_position(void)
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last_loiter_ms = now;
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// setup vertical speed and acceleration
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pos_control->set_max_speed_z(-pilot_velocity_z_max, pilot_velocity_z_max);
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pos_control->set_max_speed_z(-get_pilot_velocity_z_max_dn(), pilot_velocity_z_max_up);
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pos_control->set_max_accel_z(pilot_accel_z);
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// setup horizontal speed and acceleration
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@ -2831,7 +2843,7 @@ bool QuadPlane::do_vtol_takeoff(const AP_Mission::Mission_Command& cmd)
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loiter_nav->init_target();
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// initialize vertical speed and acceleration
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pos_control->set_max_speed_z(-pilot_velocity_z_max, pilot_velocity_z_max);
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pos_control->set_max_speed_z(-get_pilot_velocity_z_max_dn(), pilot_velocity_z_max_up);
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pos_control->set_max_accel_z(pilot_accel_z);
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// initialise position and desired velocity
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@ -2851,7 +2863,7 @@ bool QuadPlane::do_vtol_takeoff(const AP_Mission::Mission_Command& cmd)
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// t = max(t_{accel}, 0) + max(t_{constant}, 0)
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const float d_total = (plane.next_WP_loc.alt - plane.current_loc.alt) * 0.01f;
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const float accel_m_s_s = MAX(10, pilot_accel_z) * 0.01f;
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const float vel_max = MAX(10, pilot_velocity_z_max) * 0.01f;
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const float vel_max = MAX(10, pilot_velocity_z_max_up) * 0.01f;
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const float vel_z = inertial_nav.get_velocity_z() * 0.01f;
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const float t_accel = (vel_max - vel_z) / accel_m_s_s;
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const float d_accel = vel_z * t_accel + 0.5f * accel_m_s_s * sq(t_accel);
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@ -3583,4 +3595,13 @@ bool QuadPlane::show_vtol_view() const
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return show_vtol;
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}
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// return the PILOT_VELZ_MAX_DN value if non zero, otherwise returns the PILOT_VELZ_MAX value.
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uint16_t QuadPlane::get_pilot_velocity_z_max_dn() const
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{
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if (pilot_velocity_z_max_dn == 0) {
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return abs(pilot_velocity_z_max_up);
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}
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return abs(pilot_velocity_z_max_dn);
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}
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QuadPlane *QuadPlane::_singleton = nullptr;
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@ -155,6 +155,8 @@ public:
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// return true if the user has set ENABLE
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bool enabled(void) const { return enable != 0; }
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uint16_t get_pilot_velocity_z_max_dn() const;
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struct PACKED log_QControl_Tuning {
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LOG_PACKET_HEADER;
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uint64_t time_us;
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@ -200,7 +202,8 @@ private:
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AC_Loiter *loiter_nav;
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// maximum vertical velocity the pilot may request
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AP_Int16 pilot_velocity_z_max;
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AP_Int16 pilot_velocity_z_max_up;
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AP_Int16 pilot_velocity_z_max_dn;
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// vertical acceleration the pilot may request
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AP_Int16 pilot_accel_z;
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