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MAV'RIC
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Configuration for quad dynamic model. More...
#include <dynamic_model_quad_diag.hpp>
Public Attributes | |
| float | rotor_lpf |
| Low-pass filtered response of the rotors to simulate inertia and lag. | |
| float | rotor_rpm_gain |
| Gain linking the command to rpm. | |
| float | rotor_rpm_offset |
| Offset to convert servo commands to rpm. | |
| float | rotor_cd |
| Rotor drag coefficient. | |
| float | rotor_cl |
| Rotor lift coefficient. | |
| float | rotor_diameter |
| Mean rotor diameter in m. | |
| float | rotor_foil_area |
| Rotor foil area. | |
| float | rotor_pitch |
| Rotor pitch. | |
| float | total_mass |
| Vehicle mass in kg. | |
| float | vehicle_drag |
| Coefficient of drag of the whole vehicle. | |
| float | roll_pitch_momentum |
| Roll and pitch angular momentum of the vehicle. | |
| float | yaw_momentum |
| Yaw angular momentum constants (assumed to be independent) | |
| float | rotor_momentum |
| Angular momentum of the rotor (for rotor inertia) | |
| float | rotor_arm_length |
| Distance between CoG and motor (in meter) | |
| float | wind_x |
| X component of wind in global frame in m/s. | |
| float | wind_y |
| Y component of wind in global frame in m/s. | |
| float | gravity |
| Gravity value used for the simulated forces. | |
| float | air_density |
| Air density in kg/m3. | |
| std::array< float, 4 > | motor_dir |
Configuration for quad dynamic model.
1.7.6.1