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MAV'RIC
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Structure containing the configuration data. More...
#include <stabilisation_wing.hpp>

Public Attributes | |
| float | thrust_apriori |
| A priori thrust. | |
| float | pitch_angle_apriori |
| Constant a priori on the pitch angle. | |
| float | pitch_angle_apriori_gain |
| Gain of the pitch angle a priori which is function of the roll value. | |
| float | max_roll_angle |
| Maximum roll value that the velocity layer could ask to follow. | |
| float | take_off_thrust |
| Thrust value used during the take-off. | |
| float | take_off_pitch |
| Pitch angle used during the take-off. | |
| float | landing_pitch |
| Pitch angle used during the landing. | |
| float | landing_max_roll |
| Maximum roll angle during landing. | |
| stabiliser_stack_wing_t | stabiliser_stack |
| The pointer to the PID parameters values and output for the stacked controller. | |
Structure containing the configuration data.
1.7.6.1