mirror of https://github.com/ArduPilot/ardupilot
50 lines
1.4 KiB
C++
50 lines
1.4 KiB
C++
#include "mode.h"
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#include "Plane.h"
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#if HAL_QUADPLANE_ENABLED
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bool ModeQHover::_enter()
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{
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// set vertical speed and acceleration limits
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pos_control->set_max_speed_accel_z(-quadplane.get_pilot_velocity_z_max_dn(), quadplane.pilot_velocity_z_max_up, quadplane.pilot_accel_z);
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pos_control->set_correction_speed_accel_z(-quadplane.get_pilot_velocity_z_max_dn(), quadplane.pilot_velocity_z_max_up, quadplane.pilot_accel_z);
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quadplane.set_climb_rate_cms(0);
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quadplane.init_throttle_wait();
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return true;
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}
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void ModeQHover::update()
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{
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plane.mode_qstabilize.update();
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}
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/*
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control QHOVER mode
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*/
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void ModeQHover::run()
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{
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const uint32_t now = AP_HAL::millis();
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if (quadplane.tailsitter.in_vtol_transition(now)) {
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// Tailsitters in FW pull up phase of VTOL transition run FW controllers
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Mode::run();
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return;
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}
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if (quadplane.throttle_wait) {
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quadplane.set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE);
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attitude_control->set_throttle_out(0, true, 0);
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quadplane.relax_attitude_control();
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pos_control->relax_z_controller(0);
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} else {
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plane.quadplane.assign_tilt_to_fwd_thr();
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quadplane.hold_hover(quadplane.get_pilot_desired_climb_rate_cms());
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}
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// Stabilize with fixed wing surfaces
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plane.stabilize_roll();
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plane.stabilize_pitch();
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}
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#endif
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