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[paparazzi-commits] [6357] cleanup some trailing whitespaces
|
From: |
Felix Ruess |
|
Subject: |
[paparazzi-commits] [6357] cleanup some trailing whitespaces |
|
Date: |
Fri, 05 Nov 2010 16:24:31 +0000 |
Revision: 6357
http://svn.sv.gnu.org/viewvc/?view=rev&root=paparazzi&revision=6357
Author: flixr
Date: 2010-11-05 16:24:29 +0000 (Fri, 05 Nov 2010)
Log Message:
-----------
cleanup some trailing whitespaces
Modified Paths:
--------------
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v.c
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v.h
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.c
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.h
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.c
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.h
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.h
Modified: paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v.c
===================================================================
--- paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v.c
2010-11-05 16:24:18 UTC (rev 6356)
+++ paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v.c
2010-11-05 16:24:29 UTC (rev 6357)
@@ -1,6 +1,6 @@
/*
* $Id$
- *
+ *
* Copyright (C) 2006 Pascal Brisset, Antoine Drouin, Michel Gorraz
*
* This file is part of paparazzi.
@@ -18,11 +18,11 @@
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
- * Boston, MA 02111-1307, USA.
+ * Boston, MA 02111-1307, USA.
*
*/
-/**
+/**
* \file v_ctl_ctl
* \brief Vertical control for fixed wing vehicles.
*
@@ -123,14 +123,14 @@
/* "auto throttle" inner loop parameters */
v_ctl_auto_throttle_nominal_cruise_throttle =
V_CTL_AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE;
v_ctl_auto_throttle_cruise_throttle =
v_ctl_auto_throttle_nominal_cruise_throttle;
- v_ctl_auto_throttle_climb_throttle_increment =
+ v_ctl_auto_throttle_climb_throttle_increment =
V_CTL_AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT;
v_ctl_auto_throttle_pgain = V_CTL_AUTO_THROTTLE_PGAIN;
v_ctl_auto_throttle_igain = V_CTL_AUTO_THROTTLE_IGAIN;
v_ctl_auto_throttle_dgain = 0.;
v_ctl_auto_throttle_sum_err = 0.;
- v_ctl_auto_throttle_pitch_of_vz_pgain =
V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_PGAIN;
- v_ctl_auto_throttle_pitch_of_vz_dgain =
V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_DGAIN;
+ v_ctl_auto_throttle_pitch_of_vz_pgain =
V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_PGAIN;
+ v_ctl_auto_throttle_pitch_of_vz_dgain =
V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_DGAIN;
#ifdef V_CTL_AUTO_PITCH_PGAIN
/* "auto pitch" inner loop parameters */
@@ -161,7 +161,7 @@
#define AGR_CLIMB_THROTTLE agr_climb_throttle
agr_climb_pitch = AGR_CLIMB_PITCH;
#undef AGR_CLIMB_PITCH
- #define AGR_CLIMB_PITCH agr_climb_pitch
+ #define AGR_CLIMB_PITCH agr_climb_pitch
agr_climb_nav_ratio = AGR_CLIMB_NAV_RATIO;
#undef AGR_CLIMB_NAV_RATIO
#define AGR_CLIMB_NAV_RATIO agr_climb_nav_ratio
@@ -177,9 +177,9 @@
#endif
}
-/**
+/**
* outer loop
- * \brief Computes v_ctl_climb_setpoint and sets v_ctl_auto_throttle_submode
+ * \brief Computes v_ctl_climb_setpoint and sets v_ctl_auto_throttle_submode
*/
void v_ctl_altitude_loop( void ) {
float altitude_pgain_boost = 1.0;
@@ -228,9 +228,9 @@
}
}
-/**
+/**
* auto throttle inner loop
- * \brief
+ * \brief
*/
#ifndef USE_AIRSPEED
@@ -242,12 +242,12 @@
float err = estimator_z_dot - v_ctl_climb_setpoint;
float d_err = err - last_err;
last_err = err;
- float controlled_throttle = v_ctl_auto_throttle_cruise_throttle
- + v_ctl_auto_throttle_climb_throttle_increment * v_ctl_climb_setpoint
- + v_ctl_auto_throttle_pgain *
+ float controlled_throttle = v_ctl_auto_throttle_cruise_throttle
+ + v_ctl_auto_throttle_climb_throttle_increment * v_ctl_climb_setpoint
+ + v_ctl_auto_throttle_pgain *
(err + v_ctl_auto_throttle_igain * v_ctl_auto_throttle_sum_err
+ v_ctl_auto_throttle_dgain * d_err);
-
+
/* pitch pre-command */
float v_ctl_pitch_of_vz = (v_ctl_climb_setpoint + d_err *
v_ctl_auto_throttle_pitch_of_vz_dgain) * v_ctl_auto_throttle_pitch_of_vz_pgain;
@@ -257,15 +257,15 @@
if (v_ctl_climb_setpoint > 0) { /* Climbing */
f_throttle = AGR_CLIMB_THROTTLE;
nav_pitch = AGR_CLIMB_PITCH;
- }
+ }
else { /* Going down */
f_throttle = AGR_DESCENT_THROTTLE;
nav_pitch = AGR_DESCENT_PITCH;
}
break;
-
+
case V_CTL_AUTO_THROTTLE_BLENDED: {
- float ratio = (fabs(v_ctl_altitude_error) - AGR_BLEND_END)
+ float ratio = (fabs(v_ctl_altitude_error) - AGR_BLEND_END)
/ (AGR_BLEND_START - AGR_BLEND_END);
f_throttle = (1-ratio) * controlled_throttle;
nav_pitch = (1-ratio) * v_ctl_pitch_of_vz;
@@ -280,7 +280,7 @@
}
break;
}
-
+
case V_CTL_AUTO_THROTTLE_STANDARD:
default:
#endif
@@ -346,7 +346,7 @@
#endif // USE_AIRSPEED
-/**
+/**
* auto pitch inner loop
* \brief computes a nav_pitch from a climb_setpoint given a fixed throttle
*/
@@ -356,7 +356,7 @@
v_ctl_throttle_setpoint = nav_throttle_setpoint;
v_ctl_auto_pitch_sum_err += err;
BoundAbs(v_ctl_auto_pitch_sum_err, V_CTL_AUTO_PITCH_MAX_SUM_ERR);
- nav_pitch = v_ctl_auto_pitch_pgain *
+ nav_pitch = v_ctl_auto_pitch_pgain *
(err + v_ctl_auto_pitch_igain * v_ctl_auto_pitch_sum_err);
Bound(nav_pitch, V_CTL_AUTO_PITCH_MIN_PITCH, V_CTL_AUTO_PITCH_MAX_PITCH);
}
Modified: paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v.h
===================================================================
--- paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v.h
2010-11-05 16:24:18 UTC (rev 6356)
+++ paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v.h
2010-11-05 16:24:29 UTC (rev 6357)
@@ -1,6 +1,6 @@
/*
* Paparazzi $Id$
- *
+ *
* Copyright (C) 2006 Pascal Brisset, Antoine Drouin
*
* This file is part of paparazzi.
@@ -18,11 +18,11 @@
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
- * Boston, MA 02111-1307, USA.
+ * Boston, MA 02111-1307, USA.
*
*/
-/**
+/**
*
* fixed wing vertical control
*
@@ -51,7 +51,7 @@
/* inner loop */
extern float v_ctl_climb_setpoint;
extern uint8_t v_ctl_climb_mode;
-#define V_CTL_CLIMB_MODE_AUTO_THROTTLE 0
+#define V_CTL_CLIMB_MODE_AUTO_THROTTLE 0
#define V_CTL_CLIMB_MODE_AUTO_PITCH 1
extern uint8_t v_ctl_auto_throttle_submode;
Modified:
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.c
===================================================================
--- paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.c
2010-11-05 16:24:18 UTC (rev 6356)
+++ paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.c
2010-11-05 16:24:29 UTC (rev 6357)
@@ -1,6 +1,6 @@
/*
* $Id: $
- *
+ *
* Copyright (C) 2010 ENAC
*
* This file is part of paparazzi.
@@ -18,11 +18,11 @@
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
- * Boston, MA 02111-1307, USA.
+ * Boston, MA 02111-1307, USA.
*
*/
-/**
+/**
* \file v_ctl_ctl_n
* \brief Vertical control for fixed wing vehicles.
*
@@ -120,8 +120,8 @@
v_ctl_auto_throttle_igain = V_CTL_AUTO_THROTTLE_IGAIN;
v_ctl_auto_throttle_dgain = 0.;
v_ctl_auto_throttle_sum_err = 0.;
- v_ctl_auto_throttle_pitch_of_vz_pgain =
V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_PGAIN;
- v_ctl_auto_throttle_pitch_of_vz_dgain =
V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_DGAIN;
+ v_ctl_auto_throttle_pitch_of_vz_pgain =
V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_PGAIN;
+ v_ctl_auto_throttle_pitch_of_vz_dgain =
V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_DGAIN;
/* "auto pitch" inner loop parameters */
v_ctl_auto_pitch_pgain = V_CTL_AUTO_PITCH_PGAIN;
@@ -146,9 +146,9 @@
v_ctl_throttle_setpoint = 0;
}
-/**
+/**
* outer loop
- * \brief Computes v_ctl_climb_setpoint and sets v_ctl_auto_throttle_submode
+ * \brief Computes v_ctl_climb_setpoint and sets v_ctl_auto_throttle_submode
*/
// Don't use lead controller unless you know what you're doing
@@ -172,7 +172,7 @@
float diff_climb = v_ctl_climb_setpoint - v_ctl_climb_setpoint_last;
BoundAbs(diff_climb, V_CTL_AUTO_CLIMB_LIMIT);
v_ctl_climb_setpoint = v_ctl_climb_setpoint_last + diff_climb;
-
+
// Limit climb setpoint
BoundAbs(v_ctl_climb_setpoint, V_CTL_ALTITUDE_MAX_CLIMB);
v_ctl_climb_setpoint_last = v_ctl_climb_setpoint;
@@ -289,4 +289,3 @@
BoundAbs(diff_throttle, TRIM_PPRZ(V_CTL_THROTTLE_SLEW*MAX_PPRZ));
v_ctl_throttle_slewed += diff_throttle;
}
-
Modified:
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.h
===================================================================
--- paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.h
2010-11-05 16:24:18 UTC (rev 6356)
+++ paparazzi3/trunk/sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.h
2010-11-05 16:24:29 UTC (rev 6357)
@@ -1,6 +1,6 @@
/*
* $Id: $
- *
+ *
* Copyright (C) 2010 ENAC
*
* This file is part of paparazzi.
@@ -18,11 +18,11 @@
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
- * Boston, MA 02111-1307, USA.
+ * Boston, MA 02111-1307, USA.
*
*/
-/**
+/**
*
* fixed wing vertical control
*
Modified:
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.c
===================================================================
---
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.c
2010-11-05 16:24:18 UTC (rev 6356)
+++
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.c
2010-11-05 16:24:29 UTC (rev 6357)
@@ -1,6 +1,6 @@
/*
* Paparazzi $Id: fw_h_ctl.c 3603 2009-07-01 20:06:53Z hecto $
- *
+ *
* Copyright (C) 2009-2010 The Paparazzi Team
*
* This file is part of paparazzi.
@@ -18,11 +18,11 @@
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
- * Boston, MA 02111-1307, USA.
+ * Boston, MA 02111-1307, USA.
*
*/
-/**
+/**
*
* fixed wing horizontal adaptive control
*
@@ -150,8 +150,8 @@
}
-/**
- * \brief
+/**
+ * \brief
*
*/
void h_ctl_course_loop ( void ) {
@@ -165,7 +165,7 @@
last_err = err;
NormRadAngle(d_err);
- float speed_depend_nav = estimator_hspeed_mod/NOMINAL_AIRSPEED;
+ float speed_depend_nav = estimator_hspeed_mod/NOMINAL_AIRSPEED;
Bound(speed_depend_nav, 0.66, 1.5);
h_ctl_roll_setpoint = h_ctl_course_pre_bank_correction *
h_ctl_course_pre_bank
@@ -264,7 +264,7 @@
//x cmd /= airspeed_ratio2;
// Set aileron commands
- h_ctl_aileron_setpoint = TRIM_PPRZ(cmd);
+ h_ctl_aileron_setpoint = TRIM_PPRZ(cmd);
}
@@ -342,4 +342,3 @@
h_ctl_elevator_setpoint = TRIM_PPRZ(cmd);
}
-
Modified:
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.h
===================================================================
---
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.h
2010-11-05 16:24:18 UTC (rev 6356)
+++
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.h
2010-11-05 16:24:29 UTC (rev 6357)
@@ -1,6 +1,6 @@
/*
* Paparazzi $Id: fw_h_ctl.h 3784 2009-07-24 14:55:54Z poine $
- *
+ *
* Copyright (C) 2009 ENAC
*
* This file is part of paparazzi.
@@ -18,11 +18,11 @@
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
- * Boston, MA 02111-1307, USA.
+ * Boston, MA 02111-1307, USA.
*
*/
-/**
+/**
*
* fixed wing horizontal adaptive control
*
Modified:
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c
===================================================================
---
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c
2010-11-05 16:24:18 UTC (rev 6356)
+++
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c
2010-11-05 16:24:29 UTC (rev 6357)
@@ -1,6 +1,6 @@
/*
* Paparazzi $Id$
- *
+ *
* Copyright (C) 2006 Pascal Brisset, Antoine Drouin, Michel Gorraz
*
* This file is part of paparazzi.
@@ -18,11 +18,11 @@
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
- * Boston, MA 02111-1307, USA.
+ * Boston, MA 02111-1307, USA.
*
*/
-/**
+/**
*
* fixed wing horizontal control
*
@@ -164,8 +164,8 @@
#endif
}
-/**
- * \brief
+/**
+ * \brief
*
*/
void h_ctl_course_loop ( void ) {
@@ -180,7 +180,7 @@
const float reference_advance = (NOMINAL_AIRSPEED / 2.);
float advance = cos(err) * estimator_hspeed_mod / reference_advance;
- if (
+ if (
(advance < 1.) && // Path speed is small
(estimator_hspeed_mod < reference_advance) // Small path speed is due
to wind (small groundspeed)
)
@@ -203,12 +203,12 @@
// Heading error
float herr = estimator_psi - h_ctl_course_setpoint; //+crab);
NormRadAngle(herr);
-
+
if (advance < -0.5) //<! moving in the wrong direction / big
> 90 degree turn
{
err = herr;
}
- else if (advance < 0.) //<!
+ else if (advance < 0.) //<!
{
err = (-advance)*2. * herr;
}
@@ -259,7 +259,7 @@
}
#endif
- float speed_depend_nav = estimator_hspeed_mod/NOMINAL_AIRSPEED;
+ float speed_depend_nav = estimator_hspeed_mod/NOMINAL_AIRSPEED;
Bound(speed_depend_nav, 0.66, 1.5);
float cmd = h_ctl_course_pgain * speed_depend_nav * (err + d_err *
h_ctl_course_dgain);
@@ -272,11 +272,11 @@
if (v_ctl_auto_throttle_submode == V_CTL_AUTO_THROTTLE_AGRESSIVE ||
V_CTL_AUTO_THROTTLE_BLENDED) {
BoundAbs(cmd, h_ctl_roll_max_setpoint); /* bound cmd before NAV_RATIO
and again after */
if (v_ctl_altitude_error < 0) {
- nav_ratio = AGR_CLIMB_NAV_RATIO + (1 - AGR_CLIMB_NAV_RATIO) * (1 -
(fabs(v_ctl_altitude_error) - AGR_BLEND_END) / (AGR_BLEND_START -
AGR_BLEND_END));
- Bound (nav_ratio, AGR_CLIMB_NAV_RATIO, 1);
+ nav_ratio = AGR_CLIMB_NAV_RATIO + (1 - AGR_CLIMB_NAV_RATIO) * (1 -
(fabs(v_ctl_altitude_error) - AGR_BLEND_END) / (AGR_BLEND_START -
AGR_BLEND_END));
+ Bound (nav_ratio, AGR_CLIMB_NAV_RATIO, 1);
} else {
- nav_ratio = AGR_DESCENT_NAV_RATIO + (1 - AGR_DESCENT_NAV_RATIO) * (1 -
(fabs(v_ctl_altitude_error) - AGR_BLEND_END) / (AGR_BLEND_START -
AGR_BLEND_END));
- Bound (nav_ratio, AGR_DESCENT_NAV_RATIO, 1);
+ nav_ratio = AGR_DESCENT_NAV_RATIO + (1 - AGR_DESCENT_NAV_RATIO) * (1 -
(fabs(v_ctl_altitude_error) - AGR_BLEND_END) / (AGR_BLEND_START -
AGR_BLEND_END));
+ Bound (nav_ratio, AGR_DESCENT_NAV_RATIO, 1);
}
cmd *= nav_ratio;
}
@@ -316,7 +316,7 @@
- h_ctl_roll_rate_gain * estimator_p
+ v_ctl_throttle_setpoint * h_ctl_aileron_of_throttle;
- h_ctl_aileron_setpoint = TRIM_PPRZ(cmd);
+ h_ctl_aileron_setpoint = TRIM_PPRZ(cmd);
}
#else // H_CTL_ROLL_ATTITUDE_GAIN
@@ -324,7 +324,7 @@
/** Computes h_ctl_aileron_setpoint from h_ctl_roll_setpoint */
inline static void h_ctl_roll_loop( void ) {
float err = estimator_phi - h_ctl_roll_setpoint;
- float cmd = h_ctl_roll_pgain * err
+ float cmd = h_ctl_roll_pgain * err
+ v_ctl_throttle_setpoint * h_ctl_aileron_of_throttle;
h_ctl_aileron_setpoint = TRIM_PPRZ(cmd);
@@ -336,7 +336,7 @@
} else {
h_ctl_roll_rate_setpoint = h_ctl_roll_rate_setpoint_pgain * err;
BoundAbs(h_ctl_roll_rate_setpoint, H_CTL_ROLL_RATE_MAX_SETPOINT);
-
+
float saved_aileron_setpoint = h_ctl_aileron_setpoint;
h_ctl_roll_rate_loop();
h_ctl_aileron_setpoint = Blend(h_ctl_aileron_setpoint,
saved_aileron_setpoint, h_ctl_roll_rate_mode) ;
@@ -348,23 +348,23 @@
static inline void h_ctl_roll_rate_loop() {
float err = estimator_p - h_ctl_roll_rate_setpoint;
-
+
/* I term calculation */
static float roll_rate_sum_err = 0.;
static uint8_t roll_rate_sum_idx = 0;
static float roll_rate_sum_values[H_CTL_ROLL_RATE_SUM_NB_SAMPLES];
-
+
roll_rate_sum_err -= roll_rate_sum_values[roll_rate_sum_idx];
roll_rate_sum_values[roll_rate_sum_idx] = err;
roll_rate_sum_err += err;
roll_rate_sum_idx++;
if (roll_rate_sum_idx >= H_CTL_ROLL_RATE_SUM_NB_SAMPLES) roll_rate_sum_idx =
0;
-
+
/* D term calculations */
static float last_err = 0;
float d_err = err - last_err;
last_err = err;
-
+
float throttle_dep_pgain =
Blend(h_ctl_hi_throttle_roll_rate_pgain,
h_ctl_lo_throttle_roll_rate_pgain, v_ctl_throttle_setpoint/((float)MAX_PPRZ));
float cmd = throttle_dep_pgain * ( err + h_ctl_roll_rate_igain *
roll_rate_sum_err / H_CTL_ROLL_RATE_SUM_NB_SAMPLES + h_ctl_roll_rate_dgain *
d_err);
@@ -414,7 +414,7 @@
h_ctl_elevator_of_roll = 0.;
h_ctl_pitch_loop_setpoint =
- h_ctl_pitch_setpoint
+ h_ctl_pitch_setpoint
- h_ctl_elevator_of_roll / h_ctl_pitch_pgain * fabs(estimator_phi);
float err = estimator_theta - h_ctl_pitch_loop_setpoint;
@@ -426,5 +426,3 @@
#endif
h_ctl_elevator_setpoint = TRIM_PPRZ(cmd);
}
-
-
Modified:
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.h
===================================================================
---
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.h
2010-11-05 16:24:18 UTC (rev 6356)
+++
paparazzi3/trunk/sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.h
2010-11-05 16:24:29 UTC (rev 6357)
@@ -1,6 +1,6 @@
/*
* Paparazzi $Id$
- *
+ *
* Copyright (C) 2006 Pascal Brisset, Antoine Drouin, Michel Gorraz
*
* This file is part of paparazzi.
@@ -18,11 +18,11 @@
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
- * Boston, MA 02111-1307, USA.
+ * Boston, MA 02111-1307, USA.
*
*/
-/**
+/**
*
* fixed wing horizontal control
*
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- [paparazzi-commits] [6357] cleanup some trailing whitespaces,
Felix Ruess <=