10 #ifndef CONF_STABILISATION_COPTER_H_
11 #define CONF_STABILISATION_COPTER_H_
13 #include "stabilisation_copter.h"
46 .soft_zone_width = 0.0
72 .soft_zone_width = 0.0
98 .soft_zone_width = 0.0
125 .soft_zone_width = 0.0
131 .rpy = {0.0, 0.0, 0.0},
133 .tvel = {0.0, 0.0, 0.0},
135 .control_mode = RATE_COMMAND_MODE,
136 .yaw_mode = YAW_RELATIVE,
137 .run_mode = MOTORS_OFF
143 .attitude_stabiliser={
169 .soft_zone_width = 0.0
195 .soft_zone_width = 0.0
221 .soft_zone_width = 0.0
248 .soft_zone_width = 0.0
254 .rpy = {0.0, 0.0, 0.0},
256 .tvel = {0.0, 0.0, 0.0},
258 .control_mode = RATE_COMMAND_MODE,
259 .yaw_mode = YAW_RELATIVE,
260 .run_mode = MOTORS_OFF
266 .velocity_stabiliser={
292 .soft_zone_width = 0.3
318 .soft_zone_width = 0.3
344 .soft_zone_width = 0.0
371 .soft_zone_width = 0.2
377 .rpy = {0.0, 0.0, 0.0},
379 .tvel = {0.0, 0.0, 0.0},
381 .control_mode = RATE_COMMAND_MODE,
382 .yaw_mode = YAW_RELATIVE,
383 .run_mode = MOTORS_OFF
389 .yaw_coordination_velocity=1.5
float p_gain
Proportional gain.
Definition: pid_controller.h:97
Structure containing the stacked controller.
Definition: stabilisation_copter.h:70
stabiliser_t rate_stabiliser
The rate controller structure.
Definition: stabilisation_copter.h:72
pid_controller_t rpy_controller[3]
roll pitch yaw controllers
Definition: stabilisation.h:91