Plane: move pilot throttle output up to control modes

This commit is contained in:
Iampete1 2024-01-31 15:16:30 +00:00 committed by Andrew Tridgell
parent b1ddbe9904
commit 2f42f55278
8 changed files with 44 additions and 16 deletions

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@ -259,6 +259,21 @@ void Mode::output_rudder_and_steering(float val)
SRV_Channels::set_output_scaled(SRV_Channel::k_steering, val); SRV_Channels::set_output_scaled(SRV_Channel::k_steering, val);
} }
// Output pilot throttle, this is used in stabilized modes without auto throttle control
// Direct mapping if THR_PASS_STAB is set
// Otherwise apply curve for trim correction if configured
void Mode::output_pilot_throttle()
{
if (plane.g.throttle_passthru_stabilize) {
// THR_PASS_STAB set, direct mapping
SRV_Channels::set_output_scaled(SRV_Channel::k_throttle, plane.get_throttle_input(true));
return;
}
// get throttle, but adjust center to output TRIM_THROTTLE if flight option set
SRV_Channels::set_output_scaled(SRV_Channel::k_throttle, plane.get_adjusted_throttle_input(true));
}
// true if throttle min/max limits should be applied // true if throttle min/max limits should be applied
bool Mode::use_throttle_limits() const bool Mode::use_throttle_limits() const
{ {

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@ -155,6 +155,9 @@ protected:
// Helper to output to both k_rudder and k_steering servo functions // Helper to output to both k_rudder and k_steering servo functions
void output_rudder_and_steering(float val); void output_rudder_and_steering(float val);
// Output pilot throttle, this is used in stabilized modes without auto throttle control
void output_pilot_throttle();
#if HAL_QUADPLANE_ENABLED #if HAL_QUADPLANE_ENABLED
// References for convenience, used by QModes // References for convenience, used by QModes
AC_PosControl*& pos_control; AC_PosControl*& pos_control;
@ -262,6 +265,8 @@ public:
bool mode_allows_autotuning() const override { return true; } bool mode_allows_autotuning() const override { return true; }
void run() override;
protected: protected:
bool _enter() override; bool _enter() override;
@ -493,6 +498,8 @@ public:
bool mode_allows_autotuning() const override { return true; } bool mode_allows_autotuning() const override { return true; }
void run() override;
}; };
class ModeFBWB : public Mode class ModeFBWB : public Mode

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@ -26,6 +26,8 @@ void ModeAcro::update()
void ModeAcro::run() void ModeAcro::run()
{ {
output_pilot_throttle();
if (plane.g.acro_locking == 2 && plane.g.acro_yaw_rate > 0 && if (plane.g.acro_locking == 2 && plane.g.acro_yaw_rate > 0 &&
plane.yawController.rate_control_enabled()) { plane.yawController.rate_control_enabled()) {
// we can do 3D acro locking // we can do 3D acro locking

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@ -14,3 +14,10 @@ void ModeAutoTune::update()
plane.mode_fbwa.update(); plane.mode_fbwa.update();
} }
void ModeAutoTune::run()
{
// Run base class function and then output throttle
Mode::run();
output_pilot_throttle();
}

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@ -35,3 +35,11 @@ void ModeFBWA::update()
} }
} }
} }
void ModeFBWA::run()
{
// Run base class function and then output throttle
Mode::run();
output_pilot_throttle();
}

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@ -13,4 +13,6 @@ void ModeStabilize::run()
plane.stabilize_pitch(); plane.stabilize_pitch();
stabilize_stick_mixing_direct(); stabilize_stick_mixing_direct();
plane.stabilize_yaw(); plane.stabilize_yaw();
output_pilot_throttle();
} }

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@ -66,4 +66,6 @@ void ModeTraining::run()
// Always manual rudder control // Always manual rudder control
output_rudder_and_steering(plane.rudder_in_expo(false)); output_rudder_and_steering(plane.rudder_in_expo(false));
output_pilot_throttle();
} }

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@ -585,23 +585,8 @@ void Plane::set_throttle(void)
#if AP_SCRIPTING_ENABLED #if AP_SCRIPTING_ENABLED
if (nav_scripting_active()) { if (nav_scripting_active()) {
SRV_Channels::set_output_scaled(SRV_Channel::k_throttle, plane.nav_scripting.throttle_pct); SRV_Channels::set_output_scaled(SRV_Channel::k_throttle, plane.nav_scripting.throttle_pct);
} else }
#endif #endif
if (control_mode == &mode_stabilize ||
control_mode == &mode_training ||
control_mode == &mode_acro ||
control_mode == &mode_fbwa ||
control_mode == &mode_autotune) {
// a manual throttle mode
if (g.throttle_passthru_stabilize) {
// manual pass through of throttle while in FBWA or
// STABILIZE mode with THR_PASS_STAB set
SRV_Channels::set_output_scaled(SRV_Channel::k_throttle, get_throttle_input(true));
} else {
// get throttle, but adjust center to output TRIM_THROTTLE if flight option set
SRV_Channels::set_output_scaled(SRV_Channel::k_throttle, get_adjusted_throttle_input(true));
}
}
if (control_mode->use_battery_compensation()) { if (control_mode->use_battery_compensation()) {
// Apply voltage compensation to throttle output from flight mode // Apply voltage compensation to throttle output from flight mode