Paparazzi UAS
v5.18.0_stable
Paparazzi is a free software Unmanned Aircraft System.
guidance_v_n.h
Go to the documentation of this file.
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/*
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* Copyright (C) 2010 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_V_CTL_N_H
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#define FW_V_CTL_N_H
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#include "
firmwares/fixedwing/guidance/guidance_v.h
"
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#define V_CTL_SPEED_THROTTLE 0
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#define V_CTL_SPEED_AIRSPEED 1
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#define V_CTL_SPEED_GROUNDSPEED 2
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extern
float
v_ctl_auto_pitch_dgain
;
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extern
float
v_ctl_auto_airspeed_throttle_pgain
;
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extern
float
v_ctl_auto_airspeed_throttle_dgain
;
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extern
float
v_ctl_auto_airspeed_throttle_igain
;
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extern
float
v_ctl_auto_airspeed_throttle_sum_err
;
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extern
float
v_ctl_auto_airspeed_pitch_pgain
;
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extern
float
v_ctl_auto_airspeed_pitch_dgain
;
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extern
float
v_ctl_auto_airspeed_pitch_igain
;
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extern
float
v_ctl_auto_airspeed_pitch_sum_err
;
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extern
uint8_t
v_ctl_speed_mode
;
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extern
float
v_ctl_pitch_loiter_trim
;
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extern
float
v_ctl_pitch_dash_trim
;
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#endif
/* FW_V_CTL_N_H */
v_ctl_speed_mode
uint8_t v_ctl_speed_mode
Definition:
energy_ctrl.c:135
v_ctl_auto_airspeed_pitch_dgain
float v_ctl_auto_airspeed_pitch_dgain
v_ctl_auto_airspeed_pitch_pgain
float v_ctl_auto_airspeed_pitch_pgain
v_ctl_auto_airspeed_throttle_pgain
float v_ctl_auto_airspeed_throttle_pgain
v_ctl_pitch_dash_trim
float v_ctl_pitch_dash_trim
Definition:
stabilization_adaptive.c:205
v_ctl_auto_airspeed_throttle_igain
float v_ctl_auto_airspeed_throttle_igain
uint8_t
unsigned char uint8_t
Definition:
types.h:14
v_ctl_pitch_loiter_trim
float v_ctl_pitch_loiter_trim
Definition:
stabilization_adaptive.c:204
v_ctl_auto_airspeed_throttle_dgain
float v_ctl_auto_airspeed_throttle_dgain
v_ctl_auto_pitch_dgain
float v_ctl_auto_pitch_dgain
Definition:
guidance_v_n.c:73
v_ctl_auto_airspeed_pitch_igain
float v_ctl_auto_airspeed_pitch_igain
v_ctl_auto_airspeed_pitch_sum_err
float v_ctl_auto_airspeed_pitch_sum_err
v_ctl_auto_airspeed_throttle_sum_err
float v_ctl_auto_airspeed_throttle_sum_err
guidance_v.h
sw
airborne
firmwares
fixedwing
guidance
guidance_v_n.h
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