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[airborne] removed pragma messages warning about changed signs

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This commit is contained in:
Felix Ruess
2012-08-04 15:12:58 +02:00
parent b38ca32008
commit ffd52c72a7
6 changed files with 0 additions and 18 deletions
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sw/airborne/firmwares/fixedwing/guidance/guidance_v.c
-2
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@@ -109,8 +109,6 @@ float v_ctl_auto_groundspeed_sum_err;
#define V_CTL_AUTO_AGR_CLIMB_GAIN 2.0 // altitude gain multiplier while in aggressive climb mode #define V_CTL_AUTO_AGR_CLIMB_GAIN 2.0 // altitude gain multiplier while in aggressive climb mode
#endif #endif
#pragma message "CAUTION! ALL control gains have to be positive now!"
#ifndef V_CTL_ALTITUDE_PRE_CLIMB_CORRECTION #ifndef V_CTL_ALTITUDE_PRE_CLIMB_CORRECTION
#define V_CTL_ALTITUDE_PRE_CLIMB_CORRECTION 1.0f #define V_CTL_ALTITUDE_PRE_CLIMB_CORRECTION 1.0f
#endif #endif
sw/airborne/firmwares/fixedwing/guidance/guidance_v_n.c
-2
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@@ -111,8 +111,6 @@ float v_ctl_auto_groundspeed_sum_err;
#define V_CTL_AUTO_GROUNDSPEED_MAX_SUM_ERR 100 #define V_CTL_AUTO_GROUNDSPEED_MAX_SUM_ERR 100
#endif #endif
#pragma message "CAUTION! ALL control gains have to be positive now!"
void v_ctl_init( void ) { void v_ctl_init( void ) {
/* mode */ /* mode */
v_ctl_mode = V_CTL_MODE_MANUAL; v_ctl_mode = V_CTL_MODE_MANUAL;
sw/airborne/firmwares/fixedwing/main_ap.c
-5
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@@ -81,11 +81,6 @@
#include "gpio.h" #include "gpio.h"
#include "led.h" #include "led.h"
#if defined RADIO_CONTROL
#pragma message "CAUTION! radio control roll channel input has been changed to follow aerospace sign conventions.\n You will have to change your radio control xml file to get a positive value when banking right!"
#endif
#if USE_AHRS #if USE_AHRS
#if USE_IMU #if USE_IMU
sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.c
-2
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@@ -116,8 +116,6 @@ inline static void h_ctl_pitch_loop( void );
#define H_CTL_COURSE_DGAIN 0. #define H_CTL_COURSE_DGAIN 0.
#endif #endif
#pragma message "CAUTION! ALL control gains have to be positive now!"
// Some default roll gains // Some default roll gains
// H_CTL_ROLL_ATTITUDE_GAIN needs to be define in airframe // H_CTL_ROLL_ATTITUDE_GAIN needs to be define in airframe
#ifndef H_CTL_ROLL_RATE_GAIN #ifndef H_CTL_ROLL_RATE_GAIN
sw/airborne/firmwares/fixedwing/stabilization/stabilization_attitude.c
-2
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@@ -37,8 +37,6 @@
#include CTRL_TYPE_H #include CTRL_TYPE_H
#include "firmwares/fixedwing/autopilot.h" #include "firmwares/fixedwing/autopilot.h"
#pragma message "CAUTION! ALL control gains have to be positive now!"
/* outer loop parameters */ /* outer loop parameters */
float h_ctl_course_setpoint; /* rad, CW/north */ float h_ctl_course_setpoint; /* rad, CW/north */
float h_ctl_course_pre_bank; float h_ctl_course_pre_bank;
sw/airborne/firmwares/rotorcraft/main.c
-5
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@@ -38,11 +38,6 @@
#include "firmwares/rotorcraft/commands.h" #include "firmwares/rotorcraft/commands.h"
#include "firmwares/rotorcraft/actuators.h" #include "firmwares/rotorcraft/actuators.h"
#if defined RADIO_CONTROL
#include "subsystems/radio_control.h"
#pragma message "CAUTION! RadioControl roll and yaw channel inputs have been reversed to follow aerospace sign conventions.\n You will have to change your radio control xml file to get a positive value when pushing roll stick right and a positive value when pushing yaw stick right!"
#endif
#include "subsystems/imu.h" #include "subsystems/imu.h"
#include "subsystems/gps.h" #include "subsystems/gps.h"