Paparazzi UAS
v7.0_unstable
Paparazzi is a free software Unmanned Aircraft System.
stabilization_adaptive.h
Go to the documentation of this file.
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/*
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* Copyright (C) 2009 ENAC
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*
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* This file is part of paparazzi.
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*
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* paparazzi is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 2, or (at your option)
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* any later version.
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*
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* paparazzi is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with paparazzi; see the file COPYING. If not, write to
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* the Free Software Foundation, 59 Temple Place - Suite 330,
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* Boston, MA 02111-1307, USA.
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*/
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#ifndef FW_H_CTL_A_H
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#define FW_H_CTL_A_H
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#include <inttypes.h>
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#include "
std.h
"
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#include "
paparazzi.h
"
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#include "generated/airframe.h"
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extern
float
h_ctl_roll_sum_err
;
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extern
float
h_ctl_pitch_sum_err
;
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extern
float
h_ctl_roll_igain
;
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extern
float
h_ctl_pitch_igain
;
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extern
float
h_ctl_roll_Kffa
;
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extern
float
h_ctl_roll_Kffd
;
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extern
float
h_ctl_pitch_Kffa
;
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extern
float
h_ctl_pitch_Kffd
;
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extern
float
h_ctl_pitch_of_roll
;
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#if H_CTL_YAW_LOOP
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extern
float
h_ctl_yaw_dgain;
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extern
float
h_ctl_yaw_ny_igain;
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#endif
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#define H_CTL_ROLL_SUM_ERR_MAX (MAX_PPRZ/2.)
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#define H_CTL_PITCH_SUM_ERR_MAX (MAX_PPRZ/2.)
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#define stabilization_adaptive_SetRollIGain(_gain) { \
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h_ctl_roll_sum_err = 0.; \
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h_ctl_roll_igain = _gain; \
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}
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#define stabilization_adaptive_SetPitchIGain(_gain) { \
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h_ctl_pitch_sum_err = 0.; \
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h_ctl_pitch_igain = _gain; \
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}
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extern
bool
use_airspeed_ratio
;
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#endif
/* FW_H_CTL_A_H */
paparazzi.h
use_airspeed_ratio
bool use_airspeed_ratio
Definition:
stabilization_adaptive.c:199
h_ctl_pitch_sum_err
float h_ctl_pitch_sum_err
Definition:
stabilization_adaptive.c:175
h_ctl_roll_sum_err
float h_ctl_roll_sum_err
Definition:
stabilization_adaptive.c:161
h_ctl_roll_igain
float h_ctl_roll_igain
Definition:
stabilization_adaptive.c:160
h_ctl_pitch_Kffd
float h_ctl_pitch_Kffd
Definition:
stabilization_adaptive.c:177
h_ctl_roll_Kffa
float h_ctl_roll_Kffa
Definition:
stabilization_adaptive.c:162
h_ctl_roll_Kffd
float h_ctl_roll_Kffd
Definition:
stabilization_adaptive.c:163
h_ctl_pitch_of_roll
float h_ctl_pitch_of_roll
Definition:
stabilization_adaptive.c:197
h_ctl_pitch_igain
float h_ctl_pitch_igain
Definition:
stabilization_adaptive.c:174
h_ctl_pitch_Kffa
float h_ctl_pitch_Kffa
Definition:
stabilization_adaptive.c:176
std.h
sw
airborne
firmwares
fixedwing
stabilization
stabilization_adaptive.h
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