AP_Motors: tradheli support for turbine start

This commit is contained in:
Ferruccio1984 2021-10-27 06:06:23 -07:00 committed by Randy Mackay
parent 6b962ae48b
commit 3a67b17142
4 changed files with 31 additions and 0 deletions

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@ -67,6 +67,9 @@ public:
// parameter_check - returns true if helicopter specific parameters are sensible, used for pre-arm check // parameter_check - returns true if helicopter specific parameters are sensible, used for pre-arm check
virtual bool parameter_check(bool display_msg) const; virtual bool parameter_check(bool display_msg) const;
//set turbine start flag on to initiaize starting sequence
void set_turb_start(bool turb_start) { _heliflags.start_engine = turb_start; }
// has_flybar - returns true if we have a mechical flybar // has_flybar - returns true if we have a mechical flybar
virtual bool has_flybar() const { return AP_MOTORS_HELI_NOFLYBAR; } virtual bool has_flybar() const { return AP_MOTORS_HELI_NOFLYBAR; }
@ -243,6 +246,7 @@ protected:
uint8_t takeoff_collective : 1; // true if collective is above 30% between H_COL_MID and H_COL_MAX uint8_t takeoff_collective : 1; // true if collective is above 30% between H_COL_MID and H_COL_MAX
uint8_t below_land_min_coll : 1; // true if collective is below H_COL_LAND_MIN uint8_t below_land_min_coll : 1; // true if collective is below H_COL_LAND_MIN
uint8_t rotor_spooldown_complete : 1; // true if the rotors have spooled down completely uint8_t rotor_spooldown_complete : 1; // true if the rotors have spooled down completely
uint8_t start_engine : 1;
} _heliflags; } _heliflags;
// parameters // parameters

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@ -15,6 +15,10 @@
#include <stdlib.h> #include <stdlib.h>
#include <AP_HAL/AP_HAL.h> #include <AP_HAL/AP_HAL.h>
<<<<<<< HEAD
=======
#include <GCS_MAVLink/GCS.h>
>>>>>>> 5faab0ee08... AP_Motors: tradheli support for turbine start
#include "AP_MotorsHeli_RSC.h" #include "AP_MotorsHeli_RSC.h"
#include <AP_RPM/AP_RPM.h> #include <AP_RPM/AP_RPM.h>
@ -268,6 +272,8 @@ void AP_MotorsHeli_RSC::output(RotorControlState state)
governor_reset(); governor_reset();
_autothrottle = false; _autothrottle = false;
_governor_fault = false; _governor_fault = false;
//turbine start flag on
_starting = true;
break; break;
case ROTOR_CONTROL_IDLE: case ROTOR_CONTROL_IDLE:
@ -283,6 +289,15 @@ void AP_MotorsHeli_RSC::output(RotorControlState state)
_control_output = constrain_float( _rsc_arot_bailout_pct/100.0f , 0.0f, 0.4f); _control_output = constrain_float( _rsc_arot_bailout_pct/100.0f , 0.0f, 0.4f);
} else { } else {
// set rotor control speed to idle speed parameter, this happens instantly and ignores ramping // set rotor control speed to idle speed parameter, this happens instantly and ignores ramping
if (_turbine_start && _starting == true ) {
_control_output += 0.001f;
if(_control_output >= 1.0f) {
_control_output = get_idle_output();
gcs().send_text(MAV_SEVERITY_INFO, "Turbine startup");
_starting = false;
}
} else{
if (_cooldown_time > 0) { if (_cooldown_time > 0) {
_control_output = get_idle_output() * 1.5f; _control_output = get_idle_output() * 1.5f;
_fast_idle_timer += dt; _fast_idle_timer += dt;
@ -293,6 +308,7 @@ void AP_MotorsHeli_RSC::output(RotorControlState state)
_control_output = get_idle_output(); _control_output = get_idle_output();
} }
} }
}
break; break;
case ROTOR_CONTROL_ACTIVE: case ROTOR_CONTROL_ACTIVE:

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@ -113,6 +113,9 @@ public:
// set the throttle percentage to be sent to external governor to signal that autorotation bailout ramp should be used within this instance of Heli_RSC // set the throttle percentage to be sent to external governor to signal that autorotation bailout ramp should be used within this instance of Heli_RSC
void set_ext_gov_arot_bail(int16_t pct) { _rsc_arot_bailout_pct = pct; } void set_ext_gov_arot_bail(int16_t pct) { _rsc_arot_bailout_pct = pct; }
// turbine start initialize sequence
void set_turbine_start(bool turbine_start) {_turbine_start = (bool)turbine_start; }
// output - update value to send to ESC/Servo // output - update value to send to ESC/Servo
void output(RotorControlState state); void output(RotorControlState state);
@ -145,6 +148,8 @@ private:
float _thrcrv_poly[4][4]; // spline polynomials for throttle curve interpolation float _thrcrv_poly[4][4]; // spline polynomials for throttle curve interpolation
float _collective_in; // collective in for throttle curve calculation, range 0-1.0f float _collective_in; // collective in for throttle curve calculation, range 0-1.0f
float _rotor_rpm; // rotor rpm from speed sensor for governor float _rotor_rpm; // rotor rpm from speed sensor for governor
bool _turbine_start;
bool _starting;
float _governor_output; // governor output for rotor speed control float _governor_output; // governor output for rotor speed control
bool _governor_engage; // RSC governor status flag bool _governor_engage; // RSC governor status flag
bool _autothrottle; // autothrottle status flag bool _autothrottle; // autothrottle status flag

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@ -292,6 +292,12 @@ void AP_MotorsHeli_Single::calculate_armed_scalars()
_main_rotor.use_bailout_ramp_time(_heliflags.enable_bailout); _main_rotor.use_bailout_ramp_time(_heliflags.enable_bailout);
_tail_rotor.use_bailout_ramp_time(_heliflags.enable_bailout); _tail_rotor.use_bailout_ramp_time(_heliflags.enable_bailout);
if (_heliflags.start_engine) {
_main_rotor.set_turbine_start(true);
} else {
_main_rotor.set_turbine_start(false);
}
// allow use of external governor autorotation bailout // allow use of external governor autorotation bailout
if (_main_rotor._ext_gov_arot_pct.get() > 0) { if (_main_rotor._ext_gov_arot_pct.get() > 0) {
// RSC only needs to know that the vehicle is in an autorotation if using the bailout window on an external governor // RSC only needs to know that the vehicle is in an autorotation if using the bailout window on an external governor