Copter: Change from enum to class

This commit is contained in:
muramura 2024-04-17 06:43:28 +09:00 committed by Randy Mackay
parent e5a2ba3ebc
commit 07a5f61782
8 changed files with 43 additions and 43 deletions

View File

@ -973,19 +973,19 @@ Mode::AltHoldModeState Mode::get_alt_hold_state(float target_climb_rate_cms)
switch (motors->get_spool_state()) {
case AP_Motors::SpoolState::SHUT_DOWN:
return AltHold_MotorStopped;
return AltHoldModeState::MotorStopped;
case AP_Motors::SpoolState::GROUND_IDLE:
return AltHold_Landed_Ground_Idle;
return AltHoldModeState::Landed_Ground_Idle;
default:
return AltHold_Landed_Pre_Takeoff;
return AltHoldModeState::Landed_Pre_Takeoff;
}
} else if (takeoff.running() || takeoff.triggered(target_climb_rate_cms)) {
// the aircraft is currently landed or taking off, asking for a positive climb rate and in THROTTLE_UNLIMITED
// the aircraft should progress through the take off procedure
return AltHold_Takeoff;
return AltHoldModeState::Takeoff;
} else if (!copter.ap.auto_armed || copter.ap.land_complete) {
// the aircraft is armed and landed
@ -1000,17 +1000,17 @@ Mode::AltHoldModeState Mode::get_alt_hold_state(float target_climb_rate_cms)
if (motors->get_spool_state() == AP_Motors::SpoolState::GROUND_IDLE) {
// the aircraft is waiting in ground idle
return AltHold_Landed_Ground_Idle;
return AltHoldModeState::Landed_Ground_Idle;
} else {
// the aircraft can leave the ground at any time
return AltHold_Landed_Pre_Takeoff;
return AltHoldModeState::Landed_Pre_Takeoff;
}
} else {
// the aircraft is in a flying state
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
return AltHold_Flying;
return AltHoldModeState::Flying;
}
}

View File

@ -231,12 +231,12 @@ protected:
virtual float throttle_hover() const;
// Alt_Hold based flight mode states used in Alt_Hold, Loiter, and Sport
enum AltHoldModeState {
AltHold_MotorStopped,
AltHold_Takeoff,
AltHold_Landed_Ground_Idle,
AltHold_Landed_Pre_Takeoff,
AltHold_Flying
enum class AltHoldModeState {
MotorStopped,
Takeoff,
Landed_Ground_Idle,
Landed_Pre_Takeoff,
Flying
};
AltHoldModeState get_alt_hold_state(float target_climb_rate_cms);

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@ -48,22 +48,22 @@ void ModeAltHold::run()
// Alt Hold State Machine
switch (althold_state) {
case AltHold_MotorStopped:
case AltHoldModeState::MotorStopped:
attitude_control->reset_rate_controller_I_terms();
attitude_control->reset_yaw_target_and_rate(false);
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
break;
case AltHold_Landed_Ground_Idle:
case AltHoldModeState::Landed_Ground_Idle:
attitude_control->reset_yaw_target_and_rate();
FALLTHROUGH;
case AltHold_Landed_Pre_Takeoff:
case AltHoldModeState::Landed_Pre_Takeoff:
attitude_control->reset_rate_controller_I_terms_smoothly();
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
break;
case AltHold_Takeoff:
case AltHoldModeState::Takeoff:
// initiate take-off
if (!takeoff.running()) {
takeoff.start(constrain_float(g.pilot_takeoff_alt,0.0f,1000.0f));
@ -76,7 +76,7 @@ void ModeAltHold::run()
takeoff.do_pilot_takeoff(target_climb_rate);
break;
case AltHold_Flying:
case AltHoldModeState::Flying:
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
#if AP_AVOIDANCE_ENABLED

View File

@ -263,7 +263,7 @@ void ModeFlowHold::run()
// Flow Hold State Machine
switch (flowhold_state) {
case AltHold_MotorStopped:
case AltHoldModeState::MotorStopped:
copter.motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::SHUT_DOWN);
copter.attitude_control->reset_rate_controller_I_terms();
copter.attitude_control->reset_yaw_target_and_rate();
@ -271,7 +271,7 @@ void ModeFlowHold::run()
flow_pi_xy.reset_I();
break;
case AltHold_Takeoff:
case AltHoldModeState::Takeoff:
// set motors to full range
copter.motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
@ -287,16 +287,16 @@ void ModeFlowHold::run()
takeoff.do_pilot_takeoff(target_climb_rate);
break;
case AltHold_Landed_Ground_Idle:
case AltHoldModeState::Landed_Ground_Idle:
attitude_control->reset_yaw_target_and_rate();
FALLTHROUGH;
case AltHold_Landed_Pre_Takeoff:
case AltHoldModeState::Landed_Pre_Takeoff:
attitude_control->reset_rate_controller_I_terms_smoothly();
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
break;
case AltHold_Flying:
case AltHoldModeState::Flying:
copter.motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
// get avoidance adjusted climb rate

View File

@ -123,7 +123,7 @@ void ModeLoiter::run()
// Loiter State Machine
switch (loiter_state) {
case AltHold_MotorStopped:
case AltHoldModeState::MotorStopped:
attitude_control->reset_rate_controller_I_terms();
attitude_control->reset_yaw_target_and_rate();
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
@ -131,18 +131,18 @@ void ModeLoiter::run()
attitude_control->input_thrust_vector_rate_heading(loiter_nav->get_thrust_vector(), target_yaw_rate, false);
break;
case AltHold_Landed_Ground_Idle:
case AltHoldModeState::Landed_Ground_Idle:
attitude_control->reset_yaw_target_and_rate();
FALLTHROUGH;
case AltHold_Landed_Pre_Takeoff:
case AltHoldModeState::Landed_Pre_Takeoff:
attitude_control->reset_rate_controller_I_terms_smoothly();
loiter_nav->init_target();
attitude_control->input_thrust_vector_rate_heading(loiter_nav->get_thrust_vector(), target_yaw_rate, false);
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
break;
case AltHold_Takeoff:
case AltHoldModeState::Takeoff:
// initiate take-off
if (!takeoff.running()) {
takeoff.start(constrain_float(g.pilot_takeoff_alt,0.0f,1000.0f));
@ -161,7 +161,7 @@ void ModeLoiter::run()
attitude_control->input_thrust_vector_rate_heading(loiter_nav->get_thrust_vector(), target_yaw_rate, false);
break;
case AltHold_Flying:
case AltHoldModeState::Flying:
// set motors to full range
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);

View File

@ -100,7 +100,7 @@ void ModePosHold::run()
// state machine
switch (poshold_state) {
case AltHold_MotorStopped:
case AltHoldModeState::MotorStopped:
attitude_control->reset_rate_controller_I_terms();
attitude_control->reset_yaw_target_and_rate(false);
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
@ -115,14 +115,14 @@ void ModePosHold::run()
init_wind_comp_estimate();
break;
case AltHold_Landed_Ground_Idle:
case AltHoldModeState::Landed_Ground_Idle:
loiter_nav->clear_pilot_desired_acceleration();
loiter_nav->init_target();
attitude_control->reset_yaw_target_and_rate();
init_wind_comp_estimate();
FALLTHROUGH;
case AltHold_Landed_Pre_Takeoff:
case AltHoldModeState::Landed_Pre_Takeoff:
attitude_control->reset_rate_controller_I_terms_smoothly();
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
@ -131,7 +131,7 @@ void ModePosHold::run()
pitch_mode = RPMode::PILOT_OVERRIDE;
break;
case AltHold_Takeoff:
case AltHoldModeState::Takeoff:
// initiate take-off
if (!takeoff.running()) {
takeoff.start(constrain_float(g.pilot_takeoff_alt,0.0f,1000.0f));
@ -152,7 +152,7 @@ void ModePosHold::run()
pitch_mode = RPMode::PILOT_OVERRIDE;
break;
case AltHold_Flying:
case AltHoldModeState::Flying:
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
// get avoidance adjusted climb rate

View File

@ -74,22 +74,22 @@ void ModeSport::run()
// State Machine
switch (sport_state) {
case AltHold_MotorStopped:
case AltHoldModeState::MotorStopped:
attitude_control->reset_rate_controller_I_terms();
attitude_control->reset_yaw_target_and_rate(false);
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
break;
case AltHold_Landed_Ground_Idle:
case AltHoldModeState::Landed_Ground_Idle:
attitude_control->reset_yaw_target_and_rate();
FALLTHROUGH;
case AltHold_Landed_Pre_Takeoff:
case AltHoldModeState::Landed_Pre_Takeoff:
attitude_control->reset_rate_controller_I_terms_smoothly();
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
break;
case AltHold_Takeoff:
case AltHoldModeState::Takeoff:
// initiate take-off
if (!takeoff.running()) {
takeoff.start(constrain_float(g.pilot_takeoff_alt,0.0f,1000.0f));
@ -102,7 +102,7 @@ void ModeSport::run()
takeoff.do_pilot_takeoff(target_climb_rate);
break;
case AltHold_Flying:
case AltHoldModeState::Flying:
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
// get avoidance adjusted climb rate

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@ -326,7 +326,7 @@ void ModeZigZag::manual_control()
// althold state machine
switch (althold_state) {
case AltHold_MotorStopped:
case AltHoldModeState::MotorStopped:
attitude_control->reset_rate_controller_I_terms();
attitude_control->reset_yaw_target_and_rate();
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
@ -334,7 +334,7 @@ void ModeZigZag::manual_control()
attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(loiter_nav->get_roll(), loiter_nav->get_pitch(), target_yaw_rate);
break;
case AltHold_Takeoff:
case AltHoldModeState::Takeoff:
// initiate take-off
if (!takeoff.running()) {
takeoff.start(constrain_float(g.pilot_takeoff_alt,0.0f,1000.0f));
@ -353,18 +353,18 @@ void ModeZigZag::manual_control()
takeoff.do_pilot_takeoff(target_climb_rate);
break;
case AltHold_Landed_Ground_Idle:
case AltHoldModeState::Landed_Ground_Idle:
attitude_control->reset_yaw_target_and_rate();
FALLTHROUGH;
case AltHold_Landed_Pre_Takeoff:
case AltHoldModeState::Landed_Pre_Takeoff:
attitude_control->reset_rate_controller_I_terms_smoothly();
loiter_nav->init_target();
attitude_control->input_thrust_vector_rate_heading(loiter_nav->get_thrust_vector(), target_yaw_rate);
pos_control->relax_z_controller(0.0f); // forces throttle output to decay to zero
break;
case AltHold_Flying:
case AltHoldModeState::Flying:
// set motors to full range
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);