diff options
Diffstat (limited to 'src/modules/uORB/topics')
18 files changed, 597 insertions, 149 deletions
diff --git a/src/modules/uORB/topics/actuator_armed.h b/src/modules/uORB/topics/actuator_armed.h new file mode 100644 index 000000000..6e944ffee --- /dev/null +++ b/src/modules/uORB/topics/actuator_armed.h @@ -0,0 +1,58 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file actuator_armed.h + * + * Actuator armed topic + * + */ + +#ifndef TOPIC_ACTUATOR_ARMED_H +#define TOPIC_ACTUATOR_ARMED_H + +#include <stdint.h> +#include "../uORB.h" + +/** global 'actuator output is live' control. */ +struct actuator_armed_s { + + uint64_t timestamp; + bool armed; /**< Set to true if system is armed */ + bool ready_to_arm; /**< Set to true if system is ready to be armed */ + bool lockdown; /**< Set to true if actuators are forced to being disabled (due to emergency or HIL) */ +}; + +ORB_DECLARE(actuator_armed); + +#endif
\ No newline at end of file diff --git a/src/modules/uORB/topics/actuator_controls.h b/src/modules/uORB/topics/actuator_controls.h index a27095be5..e768ab2f6 100644 --- a/src/modules/uORB/topics/actuator_controls.h +++ b/src/modules/uORB/topics/actuator_controls.h @@ -52,6 +52,9 @@ #define NUM_ACTUATOR_CONTROLS 8 #define NUM_ACTUATOR_CONTROL_GROUPS 4 /**< for sanity checking */ +/* control sets with pre-defined applications */ +#define ORB_ID_VEHICLE_ATTITUDE_CONTROLS ORB_ID(actuator_controls_0) + /** * @addtogroup topics * @{ @@ -72,16 +75,4 @@ ORB_DECLARE(actuator_controls_1); ORB_DECLARE(actuator_controls_2); ORB_DECLARE(actuator_controls_3); -/* control sets with pre-defined applications */ -#define ORB_ID_VEHICLE_ATTITUDE_CONTROLS ORB_ID(actuator_controls_0) - -/** global 'actuator output is live' control. */ -struct actuator_armed_s { - bool armed; /**< Set to true if system is armed */ - bool ready_to_arm; /**< Set to true if system is ready to be armed */ - bool lockdown; /**< Set to true if actuators are forced to being disabled (due to emergency or HIL) */ -}; - -ORB_DECLARE(actuator_armed); - -#endif
\ No newline at end of file +#endif diff --git a/src/modules/uORB/topics/actuator_outputs.h b/src/modules/uORB/topics/actuator_outputs.h index 30895ca83..446140423 100644 --- a/src/modules/uORB/topics/actuator_outputs.h +++ b/src/modules/uORB/topics/actuator_outputs.h @@ -60,7 +60,7 @@ struct actuator_outputs_s { uint64_t timestamp; /**< output timestamp in us since system boot */ float output[NUM_ACTUATOR_OUTPUTS]; /**< output data, in natural output units */ - int noutputs; /**< valid outputs */ + unsigned noutputs; /**< valid outputs */ }; /** diff --git a/src/modules/uORB/topics/differential_pressure.h b/src/modules/uORB/topics/differential_pressure.h index 1ffeda764..e4d2c92ce 100644 --- a/src/modules/uORB/topics/differential_pressure.h +++ b/src/modules/uORB/topics/differential_pressure.h @@ -53,6 +53,7 @@ */ struct differential_pressure_s { uint64_t timestamp; /**< microseconds since system boot, needed to integrate */ + uint64_t error_count; uint16_t differential_pressure_pa; /**< Differential pressure reading */ uint16_t max_differential_pressure_pa; /**< Maximum differential pressure reading */ float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */ diff --git a/src/modules/uORB/topics/manual_control_setpoint.h b/src/modules/uORB/topics/manual_control_setpoint.h index 261a8a4ad..eac6d6e98 100644 --- a/src/modules/uORB/topics/manual_control_setpoint.h +++ b/src/modules/uORB/topics/manual_control_setpoint.h @@ -56,17 +56,18 @@ struct manual_control_setpoint_s { float yaw; /**< rudder / yaw rate / yaw */ float throttle; /**< throttle / collective thrust / altitude */ - float manual_override_switch; /**< manual override mode (mandatory) */ - float auto_mode_switch; /**< auto mode switch (mandatory) */ + float mode_switch; /**< mode 3 position switch (mandatory): manual, assisted, auto */ + float return_switch; /**< land 2 position switch (mandatory): land, no effect */ + float assisted_switch; /**< assisted 2 position switch (optional): seatbelt, simple */ + float mission_switch; /**< mission 2 position switch (optional): mission, loiter */ /** * Any of the channels below may not be available and be set to NaN * to indicate that it does not contain valid data. */ - float manual_mode_switch; /**< manual mode (man, sas, alt) switch (optional) */ - float manual_sas_switch; /**< sas mode (rates / attitude) switch (optional) */ - float return_to_launch_switch; /**< return to launch switch (0 = disabled, 1 = enabled) */ - float auto_offboard_input_switch; /**< controller setpoint source (0 = onboard, 1 = offboard) */ + + // XXX needed or parameter? + //float auto_offboard_input_switch; /**< controller setpoint source (0 = onboard, 1 = offboard) */ float flaps; /**< flap position */ diff --git a/src/modules/uORB/topics/rc_channels.h b/src/modules/uORB/topics/rc_channels.h index e69335b3d..5a8580143 100644 --- a/src/modules/uORB/topics/rc_channels.h +++ b/src/modules/uORB/topics/rc_channels.h @@ -48,9 +48,12 @@ /** * The number of RC channel inputs supported. * Current (Q1/2013) radios support up to 18 channels, - * leaving at a sane value of 14. + * leaving at a sane value of 15. + * This number can be greater then number of RC channels, + * because single RC channel can be mapped to multiple + * functions, e.g. for various mode switches. */ -#define RC_CHANNELS_MAX 14 +#define RC_CHANNELS_MAX 15 /** * This defines the mapping of the RC functions. @@ -63,18 +66,17 @@ enum RC_CHANNELS_FUNCTION ROLL = 1, PITCH = 2, YAW = 3, - OVERRIDE = 4, - AUTO_MODE = 5, - MANUAL_MODE = 6, - SAS_MODE = 7, - RTL = 8, - OFFBOARD_MODE = 9, - FLAPS = 10, - AUX_1 = 11, - AUX_2 = 12, - AUX_3 = 13, - AUX_4 = 14, - AUX_5 = 15, + MODE = 4, + RETURN = 5, + ASSISTED = 6, + MISSION = 7, + OFFBOARD_MODE = 8, + FLAPS = 9, + AUX_1 = 10, + AUX_2 = 11, + AUX_3 = 12, + AUX_4 = 13, + AUX_5 = 14, RC_CHANNELS_FUNCTION_MAX /**< indicates the number of functions. There can be more functions than RC channels. */ }; diff --git a/src/modules/uORB/topics/safety.h b/src/modules/uORB/topics/safety.h new file mode 100644 index 000000000..a5d21cd4a --- /dev/null +++ b/src/modules/uORB/topics/safety.h @@ -0,0 +1,57 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file safety.h + * + * Safety topic to pass safety state from px4io driver to commander + * This concerns only the safety button of the px4io but has nothing to do + * with arming/disarming. + */ + +#ifndef TOPIC_SAFETY_H +#define TOPIC_SAFETY_H + +#include <stdint.h> +#include "../uORB.h" + +struct safety_s { + + uint64_t timestamp; + bool safety_switch_available; /**< Set to true if a safety switch is connected */ + bool safety_off; /**< Set to true if safety is off */ +}; + +ORB_DECLARE(safety); + +#endif
\ No newline at end of file diff --git a/src/modules/uORB/topics/servorail_status.h b/src/modules/uORB/topics/servorail_status.h new file mode 100644 index 000000000..55668790b --- /dev/null +++ b/src/modules/uORB/topics/servorail_status.h @@ -0,0 +1,67 @@ +/**************************************************************************** + * + * Copyright (C) 2012-2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file servorail_status.h + * + * Definition of the servorail status uORB topic. + */ + +#ifndef SERVORAIL_STATUS_H_ +#define SERVORAIL_STATUS_H_ + +#include "../uORB.h" +#include <stdint.h> + +/** + * @addtogroup topics + * @{ + */ + +/** + * Servorail voltages and status + */ +struct servorail_status_s { + uint64_t timestamp; /**< microseconds since system boot */ + float voltage_v; /**< Servo rail voltage in volts */ + float rssi_v; /**< RSSI pin voltage in volts */ +}; + +/** + * @} + */ + +/* register this as object request broker structure */ +ORB_DECLARE(servorail_status); + +#endif diff --git a/src/modules/uORB/topics/vehicle_attitude_setpoint.h b/src/modules/uORB/topics/vehicle_attitude_setpoint.h index a7cda34a8..1a245132a 100644 --- a/src/modules/uORB/topics/vehicle_attitude_setpoint.h +++ b/src/modules/uORB/topics/vehicle_attitude_setpoint.h @@ -64,8 +64,16 @@ struct vehicle_attitude_setpoint_s float R_body[9]; /**< Rotation matrix describing the setpoint as rotation from the current body frame */ bool R_valid; /**< Set to true if rotation matrix is valid */ + //! For quaternion-based attitude control + float q_d[4]; /** Desired quaternion for quaternion control */ + bool q_d_valid; /**< Set to true if quaternion vector is valid */ + float q_e[4]; /** Attitude error in quaternion */ + bool q_e_valid; /**< Set to true if quaternion error vector is valid */ + float thrust; /**< Thrust in Newton the power system should generate */ + bool roll_reset_integral; /**< Reset roll integral part (navigation logic change) */ + }; /** diff --git a/src/modules/uORB/topics/vehicle_command.h b/src/modules/uORB/topics/vehicle_command.h index 31ff014de..e6e4743c6 100644 --- a/src/modules/uORB/topics/vehicle_command.h +++ b/src/modules/uORB/topics/vehicle_command.h @@ -86,7 +86,8 @@ enum VEHICLE_CMD VEHICLE_CMD_OVERRIDE_GOTO=252, /* Hold / continue the current action |MAV_GOTO_DO_HOLD: hold MAV_GOTO_DO_CONTINUE: continue with next item in mission plan| MAV_GOTO_HOLD_AT_CURRENT_POSITION: Hold at current position MAV_GOTO_HOLD_AT_SPECIFIED_POSITION: hold at specified position| MAV_FRAME coordinate frame of hold point| Desired yaw angle in degrees| Latitude / X position| Longitude / Y position| Altitude / Z position| */ VEHICLE_CMD_MISSION_START=300, /* start running a mission |first_item: the first mission item to run| last_item: the last mission item to run (after this item is run, the mission ends)| */ VEHICLE_CMD_COMPONENT_ARM_DISARM=400, /* Arms / Disarms a component |1 to arm, 0 to disarm| */ - VEHICLE_CMD_ENUM_END=401, /* | */ + VEHICLE_CMD_START_RX_PAIR=500, /* Starts receiver pairing |0:Spektrum| 0:Spektrum DSM2, 1:Spektrum DSMX| */ + VEHICLE_CMD_ENUM_END=501, /* | */ }; /** @@ -119,7 +120,7 @@ struct vehicle_command_s float param5; /**< Parameter 5, as defined by MAVLink VEHICLE_CMD enum. */ float param6; /**< Parameter 6, as defined by MAVLink VEHICLE_CMD enum. */ float param7; /**< Parameter 7, as defined by MAVLink VEHICLE_CMD enum. */ - uint16_t command; /**< Command ID, as defined MAVLink by VEHICLE_CMD enum. */ + enum VEHICLE_CMD command; /**< Command ID, as defined MAVLink by VEHICLE_CMD enum. */ uint8_t target_system; /**< System which should execute the command */ uint8_t target_component; /**< Component which should execute the command, 0 for all components */ uint8_t source_system; /**< System sending the command */ diff --git a/src/modules/uORB/topics/vehicle_control_debug.h b/src/modules/uORB/topics/vehicle_control_debug.h new file mode 100644 index 000000000..6184284a4 --- /dev/null +++ b/src/modules/uORB/topics/vehicle_control_debug.h @@ -0,0 +1,87 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Author: @author Lorenz Meier <lm@inf.ethz.ch> + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file vehicle_control_debug.h + * For debugging purposes to log PID parts of controller + */ + +#ifndef TOPIC_VEHICLE_CONTROL_DEBUG_H_ +#define TOPIC_VEHICLE_CONTROL_DEBUG_H_ + +#include <stdint.h> +#include "../uORB.h" + +/** + * @addtogroup topics + * @{ + */ +struct vehicle_control_debug_s +{ + uint64_t timestamp; /**< in microseconds since system start */ + + float roll_p; /**< roll P control part */ + float roll_i; /**< roll I control part */ + float roll_d; /**< roll D control part */ + + float roll_rate_p; /**< roll rate P control part */ + float roll_rate_i; /**< roll rate I control part */ + float roll_rate_d; /**< roll rate D control part */ + + float pitch_p; /**< pitch P control part */ + float pitch_i; /**< pitch I control part */ + float pitch_d; /**< pitch D control part */ + + float pitch_rate_p; /**< pitch rate P control part */ + float pitch_rate_i; /**< pitch rate I control part */ + float pitch_rate_d; /**< pitch rate D control part */ + + float yaw_p; /**< yaw P control part */ + float yaw_i; /**< yaw I control part */ + float yaw_d; /**< yaw D control part */ + + float yaw_rate_p; /**< yaw rate P control part */ + float yaw_rate_i; /**< yaw rate I control part */ + float yaw_rate_d; /**< yaw rate D control part */ + +}; /**< vehicle_control_debug */ + + /** + * @} + */ + +/* register this as object request broker structure */ +ORB_DECLARE(vehicle_control_debug); + +#endif diff --git a/src/modules/uORB/topics/vehicle_control_mode.h b/src/modules/uORB/topics/vehicle_control_mode.h new file mode 100644 index 000000000..38fb74c9b --- /dev/null +++ b/src/modules/uORB/topics/vehicle_control_mode.h @@ -0,0 +1,93 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Author: @author Lorenz Meier <lm@inf.ethz.ch> + * @author Petri Tanskanen <petri.tanskanen@inf.ethz.ch> + * @author Thomas Gubler <thomasgubler@student.ethz.ch> + * @author Julian Oes <joes@student.ethz.ch> + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file vehicle_control_mode.h + * Definition of the vehicle_control_mode uORB topic. + * + * All control apps should depend their actions based on the flags set here. + */ + +#ifndef VEHICLE_CONTROL_MODE +#define VEHICLE_CONTROL_MODE + +#include <stdint.h> +#include <stdbool.h> +#include "../uORB.h" + +/** + * @addtogroup topics @{ + */ + + +/** + * state machine / state of vehicle. + * + * Encodes the complete system state and is set by the commander app. + */ +struct vehicle_control_mode_s +{ + uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */ + + bool flag_armed; + + bool flag_external_manual_override_ok; /**< external override non-fatal for system. Only true for fixed wing */ + + // XXX needs yet to be set by state machine helper + bool flag_system_hil_enabled; + + bool flag_control_manual_enabled; /**< true if manual input is mixed in */ + bool flag_control_offboard_enabled; /**< true if offboard control input is on */ + 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_velocity_enabled; /**< true if horizontal velocity (implies direction) is controlled */ + bool flag_control_position_enabled; /**< true if position is controlled */ + bool flag_control_altitude_enabled; /**< true if altitude is controlled */ + bool flag_control_climb_rate_enabled; /**< true if climb rate is controlled */ + + bool flag_control_auto_enabled; // TEMP + uint8_t auto_state; // TEMP navigation state for AUTO modes +}; + +/** + * @} + */ + +/* register this as object request broker structure */ +ORB_DECLARE(vehicle_control_mode); + +#endif diff --git a/src/modules/uORB/topics/vehicle_global_position.h b/src/modules/uORB/topics/vehicle_global_position.h index f036c7223..143734e37 100644 --- a/src/modules/uORB/topics/vehicle_global_position.h +++ b/src/modules/uORB/topics/vehicle_global_position.h @@ -62,18 +62,17 @@ struct vehicle_global_position_s { uint64_t timestamp; /**< time of this estimate, in microseconds since system start */ - uint64_t time_gps_usec; /**< GPS timestamp in microseconds */ - bool valid; /**< true if position satisfies validity criteria of estimator */ - - int32_t lat; /**< Latitude in 1E7 degrees LOGME */ - int32_t lon; /**< Longitude in 1E7 degrees LOGME */ - float alt; /**< Altitude in meters LOGME */ - float relative_alt; /**< Altitude above home position in meters, LOGME */ - float vx; /**< Ground X Speed (Latitude), m/s in ENU LOGME */ - float vy; /**< Ground Y Speed (Longitude), m/s in ENU LOGME */ - float vz; /**< Ground Z Speed (Altitude), m/s in ENU LOGME */ - float hdg; /**< Compass heading in radians -PI..+PI. */ + uint64_t time_gps_usec; /**< GPS timestamp in microseconds */ + bool valid; /**< true if position satisfies validity criteria of estimator */ + int32_t lat; /**< Latitude in 1E7 degrees */ + int32_t lon; /**< Longitude in 1E7 degrees */ + float alt; /**< Altitude in meters */ + float relative_alt; /**< Altitude above home position in meters, */ + float vx; /**< Ground X velocity, m/s in NED */ + float vy; /**< Ground Y velocity, m/s in NED */ + float vz; /**< Ground Z velocity, m/s in NED */ + float yaw; /**< Compass heading in radians -PI..+PI. */ }; /** diff --git a/src/modules/uORB/topics/vehicle_global_position_setpoint.h b/src/modules/uORB/topics/vehicle_global_position_setpoint.h index 5c8ce1e4d..a56434d3b 100644 --- a/src/modules/uORB/topics/vehicle_global_position_setpoint.h +++ b/src/modules/uORB/topics/vehicle_global_position_setpoint.h @@ -72,6 +72,8 @@ struct vehicle_global_position_setpoint_s float param2; float param3; float param4; + float turn_distance_xy; /**< The distance on the plane which will mark this as reached */ + float turn_distance_z; /**< The distance in Z direction which will mark this as reached */ }; /** diff --git a/src/modules/uORB/topics/vehicle_global_velocity_setpoint.h b/src/modules/uORB/topics/vehicle_global_velocity_setpoint.h new file mode 100644 index 000000000..73961cdfe --- /dev/null +++ b/src/modules/uORB/topics/vehicle_global_velocity_setpoint.h @@ -0,0 +1,64 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Author: @author Anton Babushkin <anton.babushkin@me.com> + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file vehicle_global_velocity_setpoint.h + * Definition of the global velocity setpoint uORB topic. + */ + +#ifndef TOPIC_VEHICLE_GLOBAL_VELOCITY_SETPOINT_H_ +#define TOPIC_VEHICLE_GLOBAL_VELOCITY_SETPOINT_H_ + +#include "../uORB.h" + +/** + * @addtogroup topics + * @{ + */ + +struct vehicle_global_velocity_setpoint_s +{ + float vx; /**< in m/s NED */ + float vy; /**< in m/s NED */ + float vz; /**< in m/s NED */ +}; /**< Velocity setpoint in NED frame */ + +/** + * @} + */ + +/* register this as object request broker structure */ +ORB_DECLARE(vehicle_global_velocity_setpoint); + +#endif diff --git a/src/modules/uORB/topics/vehicle_gps_position.h b/src/modules/uORB/topics/vehicle_gps_position.h index 0a7fb4e9d..1639a08c2 100644 --- a/src/modules/uORB/topics/vehicle_gps_position.h +++ b/src/modules/uORB/topics/vehicle_gps_position.h @@ -56,9 +56,9 @@ struct vehicle_gps_position_s { uint64_t timestamp_position; /**< Timestamp for position information */ - int32_t lat; /**< Latitude in 1E7 degrees */ - int32_t lon; /**< Longitude in 1E7 degrees */ - int32_t alt; /**< Altitude in 1E3 meters (millimeters) above MSL */ + int32_t lat; /**< Latitude in 1E-7 degrees */ + int32_t lon; /**< Longitude in 1E-7 degrees */ + int32_t alt; /**< Altitude in 1E-3 meters (millimeters) above MSL */ uint64_t timestamp_variance; float s_variance_m_s; /**< speed accuracy estimate m/s */ diff --git a/src/modules/uORB/topics/vehicle_local_position.h b/src/modules/uORB/topics/vehicle_local_position.h index 76eddeacd..427153782 100644 --- a/src/modules/uORB/topics/vehicle_local_position.h +++ b/src/modules/uORB/topics/vehicle_local_position.h @@ -54,27 +54,29 @@ */ struct vehicle_local_position_s { - uint64_t timestamp; /**< time of this estimate, in microseconds since system start */ - bool valid; /**< true if position satisfies validity criteria of estimator */ - - float x; /**< X positin in meters in NED earth-fixed frame */ - float y; /**< X positin in meters in NED earth-fixed frame */ - float z; /**< Z positin in meters in NED earth-fixed frame (negative altitude) */ - float absolute_alt; /**< Altitude as defined by pressure / GPS, LOGME */ - float vx; /**< Ground X Speed (Latitude), m/s in NED LOGME */ - float vy; /**< Ground Y Speed (Longitude), m/s in NED LOGME */ - float vz; /**< Ground Z Speed (Altitude), m/s in NED LOGME */ - float hdg; /**< Compass heading in radians -PI..+PI. */ - - // TODO Add covariances here - + uint64_t timestamp; /**< Time of this estimate, in microseconds since system start */ + bool xy_valid; /**< true if x and y are valid */ + bool z_valid; /**< true if z is valid */ + bool v_xy_valid; /**< true if vy and vy are valid */ + bool v_z_valid; /**< true if vz is valid */ + /* Position in local NED frame */ + float x; /**< X position in meters in NED earth-fixed frame */ + float y; /**< X position in meters in NED earth-fixed frame */ + float z; /**< Z position in meters in NED earth-fixed frame (negative altitude) */ + /* Velocity in NED frame */ + float vx; /**< Ground X Speed (Latitude), m/s in NED */ + float vy; /**< Ground Y Speed (Longitude), m/s in NED */ + float vz; /**< Ground Z Speed (Altitude), m/s in NED */ + /* Heading */ + float yaw; /* Reference position in GPS / WGS84 frame */ - uint64_t home_timestamp;/**< Time when home position was set */ - int32_t home_lat; /**< Latitude in 1E7 degrees LOGME */ - int32_t home_lon; /**< Longitude in 1E7 degrees LOGME */ - float home_alt; /**< Altitude in meters LOGME */ - float home_hdg; /**< Compass heading in radians -PI..+PI. */ - + bool xy_global; /**< true if position (x, y) is valid and has valid global reference (ref_lat, ref_lon) */ + bool z_global; /**< true if z is valid and has valid global reference (ref_alt) */ + uint64_t ref_timestamp; /**< Time when reference position was set */ + int32_t ref_lat; /**< Reference point latitude in 1E7 degrees */ + int32_t ref_lon; /**< Reference point longitude in 1E7 degrees */ + float ref_alt; /**< Reference altitude AMSL in meters, MUST be set to current (not at reference point!) ground level */ + bool landed; /**< true if vehicle is landed */ }; /** diff --git a/src/modules/uORB/topics/vehicle_status.h b/src/modules/uORB/topics/vehicle_status.h index 94068a9ac..1c184d3a7 100644 --- a/src/modules/uORB/topics/vehicle_status.h +++ b/src/modules/uORB/topics/vehicle_status.h @@ -54,22 +54,67 @@ #include <stdbool.h> #include "../uORB.h" -/* State Machine */ -typedef enum -{ - SYSTEM_STATE_PREFLIGHT = 0, - SYSTEM_STATE_STANDBY = 1, - SYSTEM_STATE_GROUND_READY = 2, - SYSTEM_STATE_MANUAL = 3, - SYSTEM_STATE_STABILIZED = 4, - SYSTEM_STATE_AUTO = 5, - SYSTEM_STATE_MISSION_ABORT = 6, - SYSTEM_STATE_EMCY_LANDING = 7, - SYSTEM_STATE_EMCY_CUTOFF = 8, - SYSTEM_STATE_GROUND_ERROR = 9, - SYSTEM_STATE_REBOOT= 10, - -} commander_state_machine_t; +/** + * @addtogroup topics @{ + */ + +/* main state machine */ +typedef enum { + MAIN_STATE_MANUAL = 0, + MAIN_STATE_SEATBELT, + MAIN_STATE_EASY, + MAIN_STATE_AUTO, +} main_state_t; + +/* navigation state machine */ +typedef enum { + NAVIGATION_STATE_DIRECT = 0, // true manual control, no any stabilization + NAVIGATION_STATE_STABILIZE, // attitude stabilization + NAVIGATION_STATE_ALTHOLD, // attitude + altitude stabilization + NAVIGATION_STATE_VECTOR, // attitude + altitude + position stabilization + NAVIGATION_STATE_AUTO_READY, // AUTO, landed, reeady for takeoff + NAVIGATION_STATE_AUTO_TAKEOFF, // detect takeoff using land detector and switch to desired AUTO mode + NAVIGATION_STATE_AUTO_LOITER, // pause mission + NAVIGATION_STATE_AUTO_MISSION, // fly mission + NAVIGATION_STATE_AUTO_RTL, // Return To Launch, when home position switch to LAND + NAVIGATION_STATE_AUTO_LAND // land and switch to AUTO_READY when landed (detect using land detector) +} navigation_state_t; + +typedef enum { + ARMING_STATE_INIT = 0, + ARMING_STATE_STANDBY, + ARMING_STATE_ARMED, + ARMING_STATE_ARMED_ERROR, + ARMING_STATE_STANDBY_ERROR, + ARMING_STATE_REBOOT, + ARMING_STATE_IN_AIR_RESTORE +} arming_state_t; + +typedef enum { + HIL_STATE_OFF = 0, + HIL_STATE_ON +} hil_state_t; + +typedef enum { + MODE_SWITCH_MANUAL = 0, + MODE_SWITCH_ASSISTED, + MODE_SWITCH_AUTO +} mode_switch_pos_t; + +typedef enum { + ASSISTED_SWITCH_SEATBELT = 0, + ASSISTED_SWITCH_EASY +} assisted_switch_pos_t; + +typedef enum { + RETURN_SWITCH_NONE = 0, + RETURN_SWITCH_RETURN +} return_switch_pos_t; + +typedef enum { + MISSION_SWITCH_NONE = 0, + MISSION_SWITCH_MISSION +} mission_switch_pos_t; enum VEHICLE_MODE_FLAG { VEHICLE_MODE_FLAG_SAFETY_ARMED = 128, @@ -82,26 +127,6 @@ enum VEHICLE_MODE_FLAG { VEHICLE_MODE_FLAG_CUSTOM_MODE_ENABLED = 1 }; /**< Same as MAV_MODE_FLAG of MAVLink 1.0 protocol */ -enum VEHICLE_FLIGHT_MODE { - VEHICLE_FLIGHT_MODE_MANUAL = 0, /**< direct manual control, exact mode determined by VEHICLE_MANUAL_CONTROL_MODE */ - VEHICLE_FLIGHT_MODE_STAB, /**< attitude or rate stabilization plus velocity or position stabilization */ - VEHICLE_FLIGHT_MODE_HOLD, /**< hold current position (hover or loiter around position when switched) */ - VEHICLE_FLIGHT_MODE_AUTO /**< attitude or rate stabilization plus absolute position control and waypoints */ -}; - -enum VEHICLE_MANUAL_CONTROL_MODE { - VEHICLE_MANUAL_CONTROL_MODE_DIRECT = 0, /**< no attitude control, direct stick input mixing (only fixed wing) */ - VEHICLE_MANUAL_CONTROL_MODE_RATES, /**< body rates control mode */ - VEHICLE_MANUAL_CONTROL_MODE_SAS /**< stability augmented system (SAS) mode */ -}; - -enum VEHICLE_MANUAL_SAS_MODE { - VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS = 0, /**< roll, pitch and yaw absolute */ - VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_RATE, /**< roll and pitch absolute, yaw rate */ - VEHICLE_MANUAL_SAS_MODE_SIMPLE, /**< simple mode (includes altitude hold) */ - VEHICLE_MANUAL_SAS_MODE_ALTITUDE /**< altitude hold */ -}; - /** * Should match 1:1 MAVLink's MAV_TYPE ENUM */ @@ -128,9 +153,9 @@ enum VEHICLE_TYPE { }; enum VEHICLE_BATTERY_WARNING { - VEHICLE_BATTERY_WARNING_NONE = 0, /**< no battery low voltage warning active */ - VEHICLE_BATTERY_WARNING_WARNING, /**< warning of low voltage 1. stage */ - VEHICLE_BATTERY_WARNING_ALERT /**< aleting of low voltage 2. stage */ + VEHICLE_BATTERY_WARNING_NONE = 0, /**< no battery low voltage warning active */ + VEHICLE_BATTERY_WARNING_LOW, /**< warning of low voltage */ + VEHICLE_BATTERY_WARNING_CRITICAL /**< alerting of critical voltage */ }; /** @@ -149,55 +174,54 @@ 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 */ - uint64_t failsave_lowlevel_start_time; /**< time when the lowlevel failsafe flag was set */ - //uint64_t failsave_highlevel_begin; TO BE COMPLETED - 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_MANUAL_CONTROL_MODE manual_control_mode; /**< current attitude control mode, as defined by VEHICLE_ATTITUDE_MODE enum */ - enum VEHICLE_MANUAL_SAS_MODE manual_sas_mode; /**< current stabilization mode */ + main_state_t main_state; /**< main state machine */ + navigation_state_t navigation_state; /**< navigation state machine */ + arming_state_t arming_state; /**< current arming state */ + hil_state_t hil_state; /**< current hil state */ + int32_t system_type; /**< system type, inspired by MAVLink's VEHICLE_TYPE enum */ int32_t system_id; /**< system id, inspired by MAVLink's system ID field */ int32_t component_id; /**< subsystem / component id, inspired by MAVLink's component ID field */ - /* system flags - these represent the state predicates */ - - bool flag_system_armed; /**< true is motors / actuators are armed */ - bool flag_control_manual_enabled; /**< true if manual input is mixed in */ - 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 flag_control_velocity_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 */ - bool flag_preflight_accel_calibration; - bool flag_preflight_airspeed_calibration; + bool is_rotary_wing; + + mode_switch_pos_t mode_switch; + return_switch_pos_t return_switch; + assisted_switch_pos_t assisted_switch; + mission_switch_pos_t mission_switch; + + bool condition_battery_voltage_valid; + bool condition_system_in_air_restore; /**< true if we can restore in mid air */ + bool condition_system_sensors_initialized; + bool condition_system_returned_to_home; + bool condition_auto_mission_available; + bool condition_global_position_valid; /**< set to true by the commander app if the quality of the gps signal is good enough to use it in the position estimator */ + bool condition_launch_position_valid; /**< indicates a valid launch position */ + bool condition_home_position_valid; /**< indicates a valid home position (a valid home position is not always a valid launch) */ + bool condition_local_position_valid; + bool condition_local_altitude_valid; + bool condition_airspeed_valid; /**< set to true by the commander app if there is a valid airspeed measurement available */ + bool condition_landed; /**< true if vehicle is landed, always true if disarmed */ bool rc_signal_found_once; - bool rc_signal_lost; /**< true if RC reception is terminally lost */ - bool rc_signal_cutting_off; /**< true if RC reception is weak / cutting off */ - uint64_t rc_signal_lost_interval; /**< interval in microseconds since when no RC signal is available */ + bool rc_signal_lost; /**< true if RC reception lost */ bool offboard_control_signal_found_once; bool offboard_control_signal_lost; bool offboard_control_signal_weak; uint64_t offboard_control_signal_lost_interval; /**< interval in microseconds without an offboard control message */ - bool failsave_lowlevel; /**< Set to true if low-level failsafe mode is enabled */ - //bool failsave_highlevel; - /* see SYS_STATUS mavlink message for the following */ uint32_t onboard_control_sensors_present; uint32_t onboard_control_sensors_enabled; uint32_t onboard_control_sensors_health; - float load; - float voltage_battery; - float current_battery; + + float load; /**< processor load from 0 to 1 */ + float battery_voltage; + float battery_current; float battery_remaining; + enum VEHICLE_BATTERY_WARNING battery_warning; /**< current battery warning mode, as defined by VEHICLE_BATTERY_WARNING enum */ uint16_t drop_rate_comm; uint16_t errors_comm; @@ -205,15 +229,6 @@ struct vehicle_status_s uint16_t errors_count2; uint16_t errors_count3; uint16_t errors_count4; - - bool flag_global_position_valid; /**< set to true by the commander app if the quality of the gps signal is good enough to use it in the position estimator */ - bool flag_local_position_valid; - bool flag_vector_flight_mode_ok; /**< position estimation, battery voltage and other critical subsystems are good for autonomous flight */ - bool flag_auto_flight_mode_ok; /**< conditions of vector flight mode apply plus a valid takeoff position lock has been aquired */ - bool flag_external_manual_override_ok; /**< external override non-fatal for system. Only true for fixed wing */ - bool flag_valid_launch_position; /**< indicates a valid launch position */ - bool flag_valid_home_position; /**< indicates a valid home position (a valid home position is not always a valid launch) */ - bool flag_airspeed_valid; /**< set to true by the commander app if there is a valid airspeed measurement available */ }; /** |