diff options
Diffstat (limited to 'src/modules/uORB/topics/position_setpoint_triplet.h')
-rw-r--r-- | src/modules/uORB/topics/position_setpoint_triplet.h | 18 |
1 files changed, 11 insertions, 7 deletions
diff --git a/src/modules/uORB/topics/position_setpoint_triplet.h b/src/modules/uORB/topics/position_setpoint_triplet.h index 8c0614f59..d9a1a4c78 100644 --- a/src/modules/uORB/topics/position_setpoint_triplet.h +++ b/src/modules/uORB/topics/position_setpoint_triplet.h @@ -60,7 +60,7 @@ enum SETPOINT_TYPE SETPOINT_TYPE_TAKEOFF, /**< takeoff setpoint */ SETPOINT_TYPE_LAND, /**< land setpoint, altitude must be ignored, descend until landing */ SETPOINT_TYPE_IDLE, /**< do nothing, switch off motors or keep at idle speed (MC) */ - SETPOINT_TYPE_OFFBOARD, /**< setpoint set by offboard */ + SETPOINT_TYPE_OFFBOARD, /**< setpoint in NED frame (x, y, z, vx, vy, vz) set by offboard */ SETPOINT_TYPE_MOVING, /**< moving setpoint, current velocity of the setpoint set */ }; @@ -72,21 +72,25 @@ struct position_setpoint_s float y; /**< local position setpoint in m in NED */ float z; /**< local position setpoint in m in NED */ bool position_valid; /**< true if local position setpoint valid */ - float vx; /**< local velocity setpoint in m in NED */ - float vy; /**< local velocity setpoint in m in NED */ - float vz; /**< local velocity setpoint in m in NED */ + float vx; /**< local velocity setpoint in m/s in NED */ + float vy; /**< local velocity setpoint in m/s in NED */ + float vz; /**< local velocity setpoint in m/s in NED */ bool velocity_valid; /**< true if local velocity setpoint valid */ double lat; /**< latitude, in deg */ double lon; /**< longitude, in deg */ float alt; /**< altitude AMSL, in m */ float yaw; /**< yaw (only for multirotors), in rad [-PI..PI), NaN = hold current yaw */ + bool yaw_valid; /**< true if yaw setpoint valid */ float yawspeed; /**< yawspeed (only for multirotors, in rad/s) */ + bool yawspeed_valid; /**< true if yawspeed setpoint valid */ float loiter_radius; /**< loiter radius (only for fixed wing), in m */ int8_t loiter_direction; /**< loiter direction: 1 = CW, -1 = CCW */ float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */ - float vel_n; /**< feed forward North velocity */ - float vel_e; /**< feed forward East velocity */ - float vel_d; /**< feed forward Downside velocity */ + float a_x; //**< acceleration x setpoint */ + float a_y; //**< acceleration y setpoint */ + float a_z; //**< acceleration z setpoint */ + bool acceleration_valid; //*< true if acceleration setpoint is valid/should be used */ + bool acceleration_is_force; //*< interprete acceleration as force */ float camera_pitch; /**< camera pitch */ }; |