Mirrors_Framework/PX4-Autopilot
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changed headers

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This commit is contained in:
Thomas Gubler
2012-10-27 18:56:45 +02:00
parent abcfe29c64
commit 56f4849e87
4 changed files with 6 additions and 4 deletions
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apps/fixedwing_att_control/fixedwing_att_control_att.c
+1 -1
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@@ -47,7 +47,7 @@
#include <math.h> #include <math.h>
#include <poll.h> #include <poll.h>
#include <time.h> #include <time.h>
#include <arch/board/up_hrt.h> #include <drivers/drv_hrt.h>
#include <arch/board/board.h> #include <arch/board/board.h>
#include <uORB/uORB.h> #include <uORB/uORB.h>
apps/fixedwing_att_control/fixedwing_att_control_main.c
+2 -1
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@@ -46,7 +46,7 @@
#include <math.h> #include <math.h>
#include <poll.h> #include <poll.h>
#include <time.h> #include <time.h>
#include <arch/board/up_hrt.h> #include <drivers/drv_hrt.h>
#include <arch/board/board.h> #include <arch/board/board.h>
#include <uORB/uORB.h> #include <uORB/uORB.h>
#include <uORB/topics/vehicle_global_position.h> #include <uORB/topics/vehicle_global_position.h>
@@ -194,6 +194,7 @@ int fixedwing_att_control_thread_main(int argc, char *argv[])
/* kill all outputs */ /* kill all outputs */
for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++) for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++)
actuators.control[i] = 0.0f; actuators.control[i] = 0.0f;
orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators); orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
apps/fixedwing_att_control/fixedwing_att_control_rate.c
+2 -1
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@@ -47,7 +47,7 @@
#include <math.h> #include <math.h>
#include <poll.h> #include <poll.h>
#include <time.h> #include <time.h>
#include <arch/board/up_hrt.h> #include <drivers/drv_hrt.h>
#include <arch/board/board.h> #include <arch/board/board.h>
#include <uORB/uORB.h> #include <uORB/uORB.h>
@@ -178,6 +178,7 @@ int fixedwing_att_control_rates(const struct vehicle_rates_setpoint_s *rate_sp,
parameters_update(&h, &p); parameters_update(&h, &p);
} }
/* Roll Rate (PI) */ /* Roll Rate (PI) */
actuators->control[0] = pid_calculate(&roll_rate_controller, rate_sp->roll, rates[0], 0, deltaT); actuators->control[0] = pid_calculate(&roll_rate_controller, rate_sp->roll, rates[0], 0, deltaT);
apps/fixedwing_pos_control/fixedwing_pos_control_main.c
+1 -1
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@@ -46,7 +46,7 @@
#include <math.h> #include <math.h>
#include <poll.h> #include <poll.h>
#include <time.h> #include <time.h>
#include <arch/board/up_hrt.h> #include <drivers/drv_hrt.h>
#include <arch/board/board.h> #include <arch/board/board.h>
#include <uORB/uORB.h> #include <uORB/uORB.h>
#include <uORB/topics/vehicle_global_position.h> #include <uORB/topics/vehicle_global_position.h>