fly316/PX4-Autopilot
7
0
Fork 0
mirror of https://gitee.com/mirrors_PX4/PX4-Autopilot.git synced 2026-11-02 01:31:36 +08:00
Code Issues Packages Projects Releases Wiki Activity

Reworking control infrastructure for inner rate loop, preparing offboard interface

Browse Source
This commit is contained in:
Lorenz Meier
2012-09-18 18:28:49 +02:00
parent 3816327977 df03433034
commit b0b72b11eb
10 changed files with 424 additions and 65 deletions
Download Patch File Download Diff File Expand all files Collapse all files
apps/uORB/topics/ardrone_motors_setpoint.h
+6 -6
View File
@@ -50,14 +50,14 @@
struct ardrone_motors_setpoint_s
{
uint16_t counter; //incremented by the writing thread everytime new data is stored
uint64_t timestamp; //in microseconds since system start, is set whenever the writing thread stores new data
uint16_t motor_front_nw; ///< Front motor in + configuration, front left motor in x configuration
uint16_t motor_right_ne; ///< Right motor in + configuration, front right motor in x configuration
uint16_t motor_back_se; ///< Back motor in + configuration, back right motor in x configuration
uint16_t motor_left_sw; ///< Left motor in + configuration, back left motor in x configuration
uint8_t group; /**< quadrotor group */
uint8_t mode; /**< requested flight mode XXX define */
float p1; /**< parameter 1: rate control: roll rate, att control: roll angle (in radians, NED) */
float p2; /**< parameter 2: rate control: pitch rate, att control: pitch angle (in radians, NED) */
float p3; /**< parameter 3: rate control: yaw rate, att control: yaw angle (in radians, NED) */
float p4; /**< parameter 4: thrust, [0..1] */
}; /**< AR.Drone low level motors */
/**
apps/uORB/topics/vehicle_status.h
+10 -9
View File
@@ -111,23 +111,24 @@ struct vehicle_status_s
uint16_t counter; /**< incremented by the writing thread everytime new data is stored */
uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */
commander_state_machine_t state_machine; /**< Current flight state, main state machine */
enum VEHICLE_FLIGHT_MODE flight_mode; /**< Current flight mode, as defined by mode switch */
enum VEHICLE_ATTITUDE_MODE attitute_mode; /**< Current attitude control mode, as defined by VEHICLE_ATTITUDE_MODE enum */
commander_state_machine_t state_machine; /**< current flight state, main state machine */
enum VEHICLE_FLIGHT_MODE flight_mode; /**< current flight mode, as defined by mode switch */
enum VEHICLE_ATTITUDE_MODE attitute_mode; /**< current attitude control mode, as defined by VEHICLE_ATTITUDE_MODE enum */
// uint8_t mode;
/* system flags - these represent the state predicates */
bool flag_system_armed; /**< True is motors / actuators are armed */
bool flag_system_armed; /**< true is motors / actuators are armed */
bool flag_control_manual_enabled; /**< true if manual input is mixed in */
bool flag_hil_enabled; /**< True if hardware in the loop simulation is enabled */
bool flag_control_offboard_enabled; /**< true if offboard control input is on */
bool flag_hil_enabled; /**< true if hardware in the loop simulation is enabled */
// bool flag_control_rates_enabled; /**< true if rates are stabilized */
// bool flag_control_attitude_enabled; *< true if attitude stabilization is mixed in
// bool control_speed_enabled; /**< true if speed (implies direction) is controlled */
// bool control_position_enabled; /**< true if position is controlled */
bool flag_control_rates_enabled; /**< true if rates are stabilized */
bool flag_control_attitude_enabled; /**< true if attitude stabilization is mixed in */
bool flag_control_speed_enabled; /**< true if speed (implies direction) is controlled */
bool flag_control_position_enabled; /**< true if position is controlled */
bool flag_preflight_gyro_calibration; /**< true if gyro calibration is requested */
bool flag_preflight_mag_calibration; /**< true if mag calibration is requested */