#include "modules/ctrl/eff_scheduling_rot_wing_V2.h"
#include "generated/airframe.h"
#include "state.h"
#include "modules/actuators/actuators.h"
#include "modules/core/abi.h"
#include "filters/low_pass_filter.h"
#include "firmwares/rotorcraft/oneloop/oneloop_andi.h"

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Macros
#define	FORCE_ONELOOP

#define	WING_ROTATION_CAN_ROT_WING_ID ABI_BROADCAST
	ABI binding wing position data. More...

Functions
void	eff_scheduling_rot_wing_update_wing_angle (void)

void	eff_scheduling_rot_wing_update_airspeed (void)

void	ele_pref_sched (void)

void	update_attitude (void)

void	sum_EFF_MAT_RW (void)
	Function that sums g1 and g2 to obtain the g1_g2 matrix. More...

void	init_RW_Model (void)

void	calc_G1_G2_RW (void)

static void	wing_position_cb (uint8_t sender_id UNUSED, struct act_feedback_t *pos_msg, uint8_t num_act)

void	eff_scheduling_rot_wing_init (void)

void	eff_scheduling_rot_wing_periodic (void)

Variables
float	actuator_state_filt_vect [EFF_MAT_COLS_NB] = {0}

float	G2_RW [EFF_MAT_COLS_NB] = {0}

float	G1_RW [EFF_MAT_ROWS_NB][EFF_MAT_COLS_NB] = {0}

float	EFF_MAT_RW [EFF_MAT_ROWS_NB][EFF_MAT_COLS_NB] = {0}

static float	flt_cut = 1.0e-4

struct FloatEulers	eulers_zxy_RW_EFF

static Butterworth2LowPass	skew_filt

bool	airspeed_fake_on = false

float	airspeed_fake = 0.0

float	ele_eff = 22.0

float	ele_min = 0.0

struct RW_Model	RW

static abi_event	wing_position_ev

float	skew_meas = 0.0

float	time = 0.0

Detailed Description

Author: Tomaso De Ponti T.M.L.nosp@m..DeP.nosp@m.onti@.nosp@m.tude.nosp@m.lft.n.nosp@m.l The control effectiveness scheduler for the rotating wing drone type

Definition in file eff_scheduling_rot_wing_V2.c.

Macro Definition Documentation

◆ FORCE_ONELOOP

#define FORCE_ONELOOP

Definition at line 33 of file eff_scheduling_rot_wing_V2.c.

◆ WING_ROTATION_CAN_ROT_WING_ID

#define WING_ROTATION_CAN_ROT_WING_ID ABI_BROADCAST

ABI binding wing position data.

Definition at line 92 of file eff_scheduling_rot_wing_V2.c.

Function Documentation

◆ calc_G1_G2_RW()

void calc_G1_G2_RW ( void )

Definition at line 218 of file eff_scheduling_rot_wing_V2.c.

References actuator_state_1l, RW_Model::ail, RW_Model::as2, RW_Model::att, I::b_xx, I::b_yy, RW_skew::cosr, RW_skew::cosr2, RW_skew::cosr3, F_M_Body::dFdu, wing_model::dLdtheta, F_M_Body::dMdu, F_M_Body::dMdud, RW_Model::ele, ele_eff, RW_Model::flp, G1_RW, G2_RW, RW_Model::I, wing_model::k0, wing_model::k1, wing_model::k2, F_M_Body::l, wing_model::L, RW_Model::m, RW_Model::mB, RW_Model::mF, RW_Model::mL, RW_Model::mP, RW_Model::mR, RW_Model::P, RW_Model::rud, RW, RW_ap, RW_aq, RW_ar, RW_aX, RW_aZ, RW_G_SCALE, RW_skew::sinr, RW_skew::sinr2, RW_skew::sinr3, RW_Model::skew, RW_Model::T, RW_attitude::theta, I::w_xx, I::w_yy, RW_Model::wing, I::xx, I::yy, and I::zz.

Referenced by eff_scheduling_rot_wing_periodic().

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◆ eff_scheduling_rot_wing_init()

void eff_scheduling_rot_wing_init ( void )

Definition at line 109 of file eff_scheduling_rot_wing_V2.c.

References init_butterworth_2_low_pass(), init_RW_Model(), skew_filt, update_attitude(), wing_position_cb(), wing_position_ev, and WING_ROTATION_CAN_ROT_WING_ID.

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◆ eff_scheduling_rot_wing_periodic()

void eff_scheduling_rot_wing_periodic ( void )

Definition at line 271 of file eff_scheduling_rot_wing_V2.c.

References calc_G1_G2_RW(), eff_scheduling_rot_wing_update_airspeed(), eff_scheduling_rot_wing_update_wing_angle(), ele_pref_sched(), sum_EFF_MAT_RW(), and update_attitude().

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◆ eff_scheduling_rot_wing_update_airspeed()

void eff_scheduling_rot_wing_update_airspeed ( void )

inline

Definition at line 382 of file eff_scheduling_rot_wing_V2.c.

References airspeed_fake, airspeed_fake_on, RW_Model::as, RW_Model::as2, RW, stateGetAirspeed_f(), and time.

Referenced by eff_scheduling_rot_wing_periodic().

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◆ eff_scheduling_rot_wing_update_wing_angle()

void eff_scheduling_rot_wing_update_wing_angle ( void )

inline

Definition at line 362 of file eff_scheduling_rot_wing_V2.c.

References RW_skew::cosr, RW_skew::cosr2, RW_skew::cosr3, RW_skew::deg, float_quat_of_eulers(), SecondOrderLowPass::o, RW_skew::rad, RW, RW_skew::sinr, RW_skew::sinr2, RW_skew::sinr3, RW_Model::skew, skew_filt, skew_meas, and update_butterworth_2_low_pass().

Referenced by eff_scheduling_rot_wing_periodic().

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◆ ele_pref_sched()

void ele_pref_sched ( void )

Definition at line 399 of file eff_scheduling_rot_wing_V2.c.

References RW_Model::as, ELE_MAX_AS, ele_min, ELE_MIN_AS, RW_Model::ele_pref, RW, and ZERO_ELE_PPRZ.

Referenced by eff_scheduling_rot_wing_periodic().

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◆ init_RW_Model()

void init_RW_Model ( void )

Definition at line 119 of file eff_scheduling_rot_wing_V2.c.

References RW_Model::ail, RW_Model::as, RW_Model::as2, RW_Model::att, I::b_xx, I::b_yy, RW_skew::cosr, RW_skew::cosr2, RW_attitude::cphi, RW_attitude::cpsi, RW_attitude::ctheta, RW_skew::deg, F_M_Body::dFdu, F_M_Body::dMdu, F_M_Body::dMdud, RW_Model::ele, ele_eff, RW_Model::ele_pref, RW_Model::flp, RW_Model::I, wing_model::k0, wing_model::k1, wing_model::k2, F_M_Body::l, RW_Model::m, RW_Model::mB, RW_Model::mF, RW_Model::mL, RW_Model::mP, RW_Model::mR, RW_attitude::phi, RW_attitude::psi, RW_skew::rad, RW_Model::rud, RW, RW_G_SCALE, RW_skew::sinr, RW_skew::sinr2, RW_skew::sinr3, RW_Model::skew, RW_attitude::sphi, RW_attitude::spsi, RW_attitude::stheta, RW_attitude::theta, I::w_xx, I::w_yy, RW_Model::wing, I::xx, I::yy, and I::zz.

Referenced by eff_scheduling_rot_wing_init().

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◆ sum_EFF_MAT_RW()

void sum_EFF_MAT_RW ( void )

Function that sums g1 and g2 to obtain the g1_g2 matrix.

It also undoes the scaling that was done to make the values readable FIXME: make this function into a for loop to make it more adaptable to different configurations

Definition at line 288 of file eff_scheduling_rot_wing_V2.c.

References RW_Model::att, RW_attitude::cphi, RW_attitude::cpsi, RW_attitude::ctheta, wing_model::dLdtheta, EFF_MAT_COLS_NB, EFF_MAT_ROWS_NB, EFF_MAT_RW, flt_cut, G1_RW, G2_RW, wing_model::L, RW_Model::m, RW_Model::P, P, RW, RW_aD, RW_aE, RW_aN, RW_ap, RW_aq, RW_ar, RW_aX, RW_aZ, RW_attitude::sphi, RW_attitude::spsi, RW_attitude::stheta, RW_Model::T, mesonh.mesonh_atmosphere::T, and RW_Model::wing.