mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-18 07:23:34 +08:00
uorb autogeneration
This commit is contained in:
committed by
Lorenz Meier
parent
3aa2297497
commit
76387b1693
@@ -1,5 +1,4 @@
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uint64 timestamp # Microseconds since system boot
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bool armed # Set to true if system is armed
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bool prearmed # Set to true if the actuator safety is disabled but motors are not armed
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bool ready_to_arm # Set to true if system is ready to be armed
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@@ -10,6 +10,9 @@ uint8 INDEX_AIRBRAKES = 6
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uint8 INDEX_LANDING_GEAR = 7
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uint8 GROUP_INDEX_ATTITUDE = 0
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uint8 GROUP_INDEX_ATTITUDE_ALTERNATE = 1
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uint64 timestamp
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uint64 timestamp_sample # the timestamp the data this control response is based on was sampled
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float32[8] control
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# TOPICS actuator_controls actuator_controls_0 actuator_controls_1 actuator_controls_2 actuator_controls_3
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# TOPICS actuator_controls_virtual_fw actuator_controls_virtual_mc
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@@ -1,5 +0,0 @@
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uint8 NUM_ACTUATOR_CONTROLS = 8
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uint8 NUM_ACTUATOR_CONTROL_GROUPS = 4
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uint64 timestamp
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uint64 timestamp_sample # the timestamp the data this control response is based on was sampled
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float32[8] control
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@@ -1,5 +0,0 @@
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uint8 NUM_ACTUATOR_CONTROLS = 8
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uint8 NUM_ACTUATOR_CONTROL_GROUPS = 4
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uint64 timestamp
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uint64 timestamp_sample # the timestamp the data this control response is based on was sampled
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float32[8] control
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@@ -1,5 +0,0 @@
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uint8 NUM_ACTUATOR_CONTROLS = 8
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uint8 NUM_ACTUATOR_CONTROL_GROUPS = 4
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uint64 timestamp
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uint64 timestamp_sample # the timestamp the data this control response is based on was sampled
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float32[8] control
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@@ -1,5 +0,0 @@
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uint8 NUM_ACTUATOR_CONTROLS = 8
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uint8 NUM_ACTUATOR_CONTROL_GROUPS = 4
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uint64 timestamp
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uint64 timestamp_sample # the timestamp the data this control response is based on was sampled
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float32[8] control
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@@ -1,4 +1,3 @@
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uint8 NUM_ACTUATORS_DIRECT = 16
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uint64 timestamp # timestamp in us since system boot
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uint32 nvalues # number of valid values
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float32[16] values # actuator values, from -1 to 1
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@@ -1,5 +1,4 @@
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uint8 NUM_ACTUATOR_OUTPUTS = 16
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uint8 NUM_ACTUATOR_OUTPUT_GROUPS = 4 # for sanity checking
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uint64 timestamp # output timestamp in us since system boot
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uint32 noutputs # valid outputs
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float32[16] output # output data, in natural output units
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@@ -1,4 +1,3 @@
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uint64 timestamp # microseconds since system boot, needed to integrate
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float32 indicated_airspeed_m_s # indicated airspeed in meters per second, -1 if unknown
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float32 true_airspeed_m_s # true filtered airspeed in meters per second, -1 if unknown
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float32 true_airspeed_unfiltered_m_s # true airspeed in meters per second, -1 if unknown
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@@ -1,4 +1,3 @@
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uint64 timestamp # microseconds since system boot, needed to integrate
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float32 voltage_v # Battery voltage in volts, 0 if unknown
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float32 voltage_filtered_v # Battery voltage in volts, filtered, 0 if unknown
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float32 current_a # Battery current in amperes, -1 if unknown
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@@ -1,4 +1,3 @@
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uint64 timestamp # Timestamp when camera was triggered
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uint32 seq # Image sequence
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@@ -14,6 +14,5 @@ uint8 MAIN_STATE_AUTO_LAND = 11
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uint8 MAIN_STATE_AUTO_FOLLOW_TARGET = 12
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uint8 MAIN_STATE_MAX = 13
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uint64 timestamp # in microseconds since system start, is set whenever the writing thread stores new data
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uint8 main_state # main state machine
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@@ -1,5 +1,4 @@
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# This is similar to the mavlink message CONTROL_SYSTEM_STATE, but for onboard use */
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uint64 timestamp # in microseconds since system start
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float32 x_acc # X acceleration in body frame
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float32 y_acc # Y acceleration in body frame
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float32 z_acc # Z acceleration in body frame
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@@ -1,4 +1,3 @@
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uint64 timestamp # Microseconds since system boot, needed to integrate
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uint64 error_count # Number of errors detected by driver
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float32 differential_pressure_raw_pa # Raw differential pressure reading (may be negative)
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float32 differential_pressure_filtered_pa # Low pass filtered differential pressure reading
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@@ -1,6 +1,5 @@
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# DISTANCE_SENSOR message data
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uint64 timestamp # Microseconds since system boot
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float32 min_distance # Minimum distance the sensor can measure (in m)
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float32 max_distance # Maximum distance the sensor can measure (in m)
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@@ -1,4 +1,3 @@
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uint64 timestamp # Timestamp in microseconds since boot
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float32[6] vel_pos_innov # velocity and position innovations
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float32[3] mag_innov # earth magnetic field innovations
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float32 heading_innov # heading innovation
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@@ -1,5 +1,4 @@
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uint8 NUM_ENCODERS = 4
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uint64 timestamp
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int64[4] counts # counts of encoder
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float32[4] velocity # counts of encoder/ second
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@@ -11,7 +11,6 @@ uint8 ESC_CONNECTION_TYPE_I2C = 3 # I2C
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uint8 ESC_CONNECTION_TYPE_CAN = 4 # CAN-Bus
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uint16 counter # incremented by the writing thread everytime new data is stored
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uint64 timestamp # in microseconds since system start, is set whenever the writing thread stores new data
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uint8 esc_count # number of connected ESCs
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uint8 esc_connectiontype # how ESCs connected to the system
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@@ -1,4 +1,3 @@
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uint64 timestamp # Timestamp in microseconds since boot
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float32[32] states # Internal filter states
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float32 n_states # Number of states effectively used
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float32[3] vibe # Vibration levels in X, Y and Z
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@@ -1,5 +1,4 @@
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# Filtered bottom flow in bodyframe.
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uint64 timestamp # time of this estimate, in microseconds since system start
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float32 sumx # Integrated bodyframe x flow in meters
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float32 sumy # Integrated bodyframe y flow in meters
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@@ -1,4 +1,3 @@
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uint64 timestamp # timestamp, UNIX epoch (GPS synced)
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float64 lat # target position (deg * 1e7)
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float64 lon # target position (deg * 1e7)
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float32 alt # target position
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@@ -1,5 +1,3 @@
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uint64 timestamp # timestamp this topic was emitted
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float32 nav_roll
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float32 nav_pitch
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float32 nav_bearing
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@@ -8,7 +8,6 @@
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#
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###############################################################################################
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uint64 timestamp # in microseconds since system start, is set whenever the writing thread stores new data
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float32 roll_body # body angle in NED frame
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float32 pitch_body # body angle in NED frame
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@@ -35,3 +34,6 @@ bool fw_control_yaw # control heading with rudder (used for auto takeoff on
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bool disable_mc_yaw_control # control yaw for mc (used for vtol weather-vane mode)
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bool apply_flaps
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# WAS vehicle_attitude_setpoint mc_virtual_attitude_setpoint fw_virtual_attitude_setpoint
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# TOPICS fw_virtual_attitude_setpoint
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@@ -8,7 +8,6 @@
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#
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###############################################################################################
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uint64 timestamp # in microseconds since system start
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float32 roll # body angular rates in NED frame
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float32 pitch # body angular rates in NED frame
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@@ -17,7 +17,6 @@ int32 MAGNETOMETER_MODE_NEGATIVE_BIAS = 2
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#
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# NOTE: Ordering of fields optimized to align to 32 bit / 4 bytes Change with consideration only
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uint64 timestamp # Timestamp in microseconds since boot, from gyro
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#
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int16[3] gyro_raw # Raw sensor values of angular velocity
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float32[3] gyro_rad_s # Angular velocity in radian per seconds
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@@ -1,5 +1,4 @@
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# GPS home position in WGS84 coordinates.
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uint64 timestamp # Timestamp (microseconds since system boot)
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float64 lat # Latitude in degrees
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float64 lon # Longitude in degrees
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@@ -12,8 +12,6 @@ int8 MODE_SLOT_5 = 4 # mode slot 5 selected
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int8 MODE_SLOT_6 = 5 # mode slot 6 selected
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int8 MODE_SLOT_MAX = 6 # number of slots plus one
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uint64 timestamp
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# Any of the channels may not be available and be set to NaN
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# to indicate that it does not contain valid data.
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# The variable names follow the definition of the
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@@ -1,4 +1,3 @@
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uint64 timestamp # Timestamp in microseconds since boot
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uint8[50] text
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uint8 severity
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@@ -1,4 +1,3 @@
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uint64 timestamp # in microseconds since system start
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float32 roll_rate_integ # roll rate inegrator
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float32 pitch_rate_integ # pitch rate integrator
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@@ -8,7 +8,6 @@
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#
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###############################################################################################
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uint64 timestamp # in microseconds since system start, is set whenever the writing thread stores new data
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float32 roll_body # body angle in NED frame
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float32 pitch_body # body angle in NED frame
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@@ -35,3 +34,6 @@ bool fw_control_yaw # control heading with rudder (used for auto takeoff on
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bool disable_mc_yaw_control # control yaw for mc (used for vtol weather-vane mode)
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bool apply_flaps
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# WAS vehicle_attitude_setpoint mc_virtual_attitude_setpoint fw_virtual_attitude_setpoint
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# TOPICS mc_virtual_attitude_setpoint
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@@ -8,7 +8,6 @@
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#
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###############################################################################################
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uint64 timestamp # in microseconds since system start
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float32 roll # body angular rates in NED frame
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float32 pitch # body angular rates in NED frame
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@@ -1,3 +1,7 @@
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int32 dataman_id # default 0, there are two offboard storage places in the dataman: 0 or 1
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uint32 count # count of the missions stored in the dataman
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int32 current_seq # default -1, start at the one changed latest
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# fixme: there is no mission definition in objects_common.cpp
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# but it's required for systemcmds/topic_listener/topic_listener
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# TOPICS mission offboard_mission onboard_mission
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@@ -1,5 +1,4 @@
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# Off-board control mode
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uint64 timestamp
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bool ignore_thrust
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bool ignore_attitude
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@@ -1,7 +1,6 @@
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# Optical flow in NED body frame in SI units.
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# @see http://en.wikipedia.org/wiki/International_System_of_Units
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uint64 timestamp # in microseconds since system start
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uint8 sensor_id # id of the sensor emitting the flow value
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float32 pixel_flow_x_integral # accumulated optical flow in radians around x axis
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float32 pixel_flow_y_integral # accumulated optical flow in radians around y axis
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@@ -1,2 +1 @@
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uint64 timestamp # time at which the latest parameter was updated
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bool saved # wether the change has already been saved to disk
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@@ -1,5 +1,4 @@
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uint64 timestamp # Microseconds since system boot
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uint64 error_count
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uint32 pulse_width # Pulse width, timer counts
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uint32 period # Period, timer counts
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@@ -1,4 +1,3 @@
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uint64 timestamp # Microseconds since system boot
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int32[100] string
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uint64 MAX_STRLEN = 100
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uint64 strlen
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+1
-1
@@ -20,7 +20,7 @@ uint8 RC_CHANNELS_FUNCTION_PARAM_2=17
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uint8 RC_CHANNELS_FUNCTION_PARAM_3_5=18
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uint8 RC_CHANNELS_FUNCTION_RATTITUDE=19
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uint8 RC_CHANNELS_FUNCTION_KILLSWITCH=20
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uint64 timestamp # Timestamp in microseconds since boot time
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uint64 timestamp_last_valid # Timestamp of last valid RC signal
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float32[18] channels # Scaled to -1..1 (throttle: 0..1)
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uint8 channel_count # Number of valid channels
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@@ -1,7 +1,6 @@
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uint8 RC_PARAM_MAP_NCHAN = 3 # This limit is also hardcoded in the enum RC_CHANNELS_FUNCTION in rc_channels.h
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uint8 PARAM_ID_LEN = 16 # corresponds to MAVLINK_MSG_PARAM_VALUE_FIELD_PARAM_ID_LEN
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uint64 timestamp # time at which the map was updated
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bool[3] valid #true for RC-Param channels which are mapped to a param
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int32[3] param_index # corresponding param index, this field is ignored if set to -1, in this case param_id will be used
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char[51] param_id # MAP_NCHAN * (ID_LEN + 1) chars, corresponding param id, null terminated
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@@ -1,5 +1,4 @@
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uint8 NUM_ACTUATOR_CONTROLS = 8
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uint8 NUM_ACTUATOR_CONTROL_GROUPS = 4
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uint64 timestamp
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uint64 timestamp_sample # the timestamp the data this control response is based on was sampled
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float32[8] control
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@@ -1,5 +1,4 @@
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uint8 NUM_ACTUATOR_CONTROLS = 8
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uint8 NUM_ACTUATOR_CONTROL_GROUPS = 4
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uint64 timestamp
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uint64 timestamp_sample # the timestamp the data this control response is based on was sampled
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float32[8] control
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@@ -1,3 +1,2 @@
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uint64 timestamp
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bool safety_switch_available # Set to true if a safety switch is connected
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bool safety_off # Set to true if safety is off
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@@ -1,6 +1,5 @@
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uint8 SAT_INFO_MAX_SATELLITES = 20
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uint64 timestamp # Timestamp of satellite info
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uint8 count # Number of satellites in satellite info
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uint8[20] svid # Space vehicle ID [1..255], see scheme below
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uint8[20] used # 0: Satellite not used, 1: used for navigation
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@@ -1,4 +1,3 @@
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uint64 timestamp
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uint64 integral_dt # integration time
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uint64 error_count
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float32 x # acceleration in the NED X board axis in m/s^2
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@@ -1,5 +1,4 @@
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float32 pressure
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float32 altitude
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float32 temperature
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uint64 timestamp
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uint64 error_count
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@@ -25,7 +25,6 @@ uint32 SENSOR_PRIO_MAX = 255
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#
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# NOTE: Ordering of fields optimized to align to 32 bit / 4 bytes Change with consideration only
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uint64 timestamp # Timestamp in microseconds since boot, from gyro
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uint64[3] gyro_timestamp # Gyro timestamps
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int16[9] gyro_raw # Raw sensor values of angular velocity
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float32[9] gyro_rad_s # Angular velocity in radian per seconds
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@@ -1,4 +1,3 @@
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uint64 timestamp
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uint64 integral_dt # integration time
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uint64 error_count
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float32 x # angular velocity in the NED X board axis in rad/s
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@@ -1,4 +1,3 @@
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uint64 timestamp
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uint64 error_count
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float32 x
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float32 y
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@@ -1,3 +1,2 @@
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uint64 timestamp # microseconds since system boot
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float32 voltage_v # Servo rail voltage in volts
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float32 rssi_v # RSSI pin voltage in volts
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@@ -1,4 +1,3 @@
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uint64 timestamp # microseconds since system boot
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float32 voltage5V_v # peripheral 5V rail voltage
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uint8 usb_connected # USB is connected when 1
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uint8 brick_valid # brick power is good when 1
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@@ -6,7 +6,6 @@ uint8 TECS_MODE_LAND_THROTTLELIM = 4
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uint8 TECS_MODE_BAD_DESCENT = 5
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uint8 TECS_MODE_CLIMBOUT = 6
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uint64 timestamp # timestamp, in microseconds since system start */
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float32 altitudeSp
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float32 altitude_filtered
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@@ -4,7 +4,6 @@ uint8 TELEMETRY_STATUS_RADIO_TYPE_UBIQUITY_BULLET = 2
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uint8 TELEMETRY_STATUS_RADIO_TYPE_WIRE = 3
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uint8 TELEMETRY_STATUS_RADIO_TYPE_USB = 4
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uint64 timestamp
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uint64 heartbeat_time # Time of last received heartbeat from remote system
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uint64 telem_time # Time of last received telemetry status packet, 0 for none
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uint8 type # type of the radio hardware
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@@ -55,7 +55,6 @@
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import genmsg.msgs
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import gencpp
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cpp_class = 'px4_%s'%spec.short_name
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native_type = '%s_s'%spec.short_name
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topic_name = spec.short_name
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}@
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@@ -74,6 +73,11 @@ topic_name = spec.short_name
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namespace px4
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{
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@[for multi_topic in topics]@
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@{
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cpp_class = 'px4_%s'%multi_topic
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}@
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||||
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class __EXPORT @(cpp_class) :
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public PX4Message<@(native_type)>
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@@ -89,7 +93,8 @@ public:
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~@(cpp_class)() {}
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static PX4TopicHandle handle() {return ORB_ID(@(topic_name));}
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static PX4TopicHandle handle() {return ORB_ID(@(multi_topic));}
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};
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@[end for]
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};
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@@ -0,0 +1,132 @@
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@###############################################
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||||
@#
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||||
@# PX4 ROS compatible message source code
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@# generation for C++
|
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@#
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@# EmPy template for generating <msg>.h files
|
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@# Based on the original template for ROS
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@#
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@###############################################
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||||
@# Start of Template
|
||||
@#
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@# Context:
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||||
@# - file_name_in (String) Source file
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@# - spec (msggen.MsgSpec) Parsed specification of the .msg file
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@# - md5sum (String) MD5Sum of the .msg specification
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@###############################################
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/****************************************************************************
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||||
*
|
||||
* Copyright (C) 2013-2015 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.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
/* Auto-generated by genmsg_cpp from file @file_name_in */
|
||||
|
||||
@{
|
||||
import genmsg.msgs
|
||||
import gencpp
|
||||
|
||||
uorb_struct = '%s_s'%spec.short_name
|
||||
uorb_pack_func = 'pack_%s'%spec.short_name
|
||||
topic_name = spec.short_name
|
||||
|
||||
type_map = {
|
||||
'int8': 'int8_t',
|
||||
'int16': 'int16_t',
|
||||
'int32': 'int32_t',
|
||||
'int64': 'int64_t',
|
||||
'uint8': 'uint8_t',
|
||||
'uint16': 'uint16_t',
|
||||
'uint32': 'uint32_t',
|
||||
'uint64': 'uint64_t',
|
||||
'float32': 'float',
|
||||
'float64': 'double',
|
||||
'bool': 'bool',
|
||||
'char': 'char',
|
||||
'fence_vertex': 'fence_vertex',
|
||||
'position_setpoint': 'position_setpoint',
|
||||
'esc_report': 'esc_report'
|
||||
}
|
||||
|
||||
msgtype_size_map = {
|
||||
'int8': 8,
|
||||
'int16': 16,
|
||||
'int32': 32,
|
||||
'int64': 64,
|
||||
'uint8': 8,
|
||||
'uint16': 16,
|
||||
'uint32': 32,
|
||||
'uint64': 64,
|
||||
'float32': 32,
|
||||
'float64': 64,
|
||||
'bool': 1,
|
||||
'char': 1,
|
||||
'fence_vertex': 8,
|
||||
'position_setpoint': 104,
|
||||
'esc_report': 36
|
||||
}
|
||||
|
||||
def convert_type(spec_type):
|
||||
bare_type = spec_type
|
||||
if '/' in spec_type:
|
||||
# removing prefix
|
||||
bare_type = (spec_type.split('/'))[1]
|
||||
|
||||
msg_type, is_array, array_length = genmsg.msgs.parse_type(bare_type)
|
||||
c_type = type_map[msg_type]
|
||||
if is_array:
|
||||
return c_type + "[" + str(array_length) + "]"
|
||||
return c_type
|
||||
|
||||
def bare_name(msg_type):
|
||||
bare = msg_type
|
||||
if '/' in msg_type:
|
||||
# removing prefix
|
||||
bare = (msg_type.split('/'))[1]
|
||||
# removing suffix
|
||||
return bare.split('[')[0]
|
||||
|
||||
def sizeof_field_type(field):
|
||||
return msgtype_size_map[bare_name(field.type)]
|
||||
|
||||
sorted_fields = sorted(spec.parsed_fields(), key = sizeof_field_type, reverse=True)
|
||||
topic_fields = ["%s %s" % (convert_type(field.type), field.name) for field in sorted_fields]
|
||||
}@
|
||||
|
||||
#include <px4_config.h>
|
||||
#include <drivers/drv_orb_dev.h>
|
||||
#include <uORB/topics/@(topic_name).h>
|
||||
|
||||
@# join all msg files in one line e.g: "float[3] position;float[3] velocity;bool armed"
|
||||
const char *__orb_@(topic_name)_fields = "@( topic_name.upper() ):@( ";".join(topic_fields) );";
|
||||
|
||||
@[for multi_topic in topics]@
|
||||
ORB_DEFINE(@multi_topic, struct @uorb_struct, __orb_@(topic_name)_fields);
|
||||
@[end for]
|
||||
@@ -75,7 +75,6 @@ for field in spec.parsed_fields():
|
||||
(package, name) = genmsg.names.package_resource_name(field.base_type)
|
||||
package = package or spec.package # convert '' to package
|
||||
print('#include <uORB/topics/%s.h>'%(name))
|
||||
|
||||
}@
|
||||
|
||||
@# Constants c style
|
||||
@@ -85,17 +84,12 @@ for field in spec.parsed_fields():
|
||||
@[end for]
|
||||
#endif
|
||||
|
||||
/**
|
||||
* @@addtogroup topics
|
||||
* @@{
|
||||
*/
|
||||
|
||||
@##############################
|
||||
@# Main struct of message
|
||||
@##############################
|
||||
@{
|
||||
|
||||
type_map = {'int8': 'int8_t',
|
||||
type_map = {
|
||||
'int8': 'int8_t',
|
||||
'int16': 'int16_t',
|
||||
'int32': 'int32_t',
|
||||
'int64': 'int64_t',
|
||||
@@ -109,37 +103,77 @@ type_map = {'int8': 'int8_t',
|
||||
'char': 'char',
|
||||
'fence_vertex': 'fence_vertex',
|
||||
'position_setpoint': 'position_setpoint',
|
||||
'esc_report': 'esc_report'}
|
||||
'esc_report': 'esc_report'
|
||||
}
|
||||
|
||||
msgtype_size_map = {
|
||||
'int8': 8,
|
||||
'int16': 16,
|
||||
'int32': 32,
|
||||
'int64': 64,
|
||||
'uint8': 8,
|
||||
'uint16': 16,
|
||||
'uint32': 32,
|
||||
'uint64': 64,
|
||||
'float32': 32,
|
||||
'float64': 64,
|
||||
'bool': 1,
|
||||
'char': 1,
|
||||
'fence_vertex': 8,
|
||||
'position_setpoint': 104,
|
||||
'esc_report': 36
|
||||
}
|
||||
|
||||
def bare_name(msg_type):
|
||||
bare = msg_type
|
||||
if '/' in msg_type:
|
||||
# removing prefix
|
||||
bare = (msg_type.split('/'))[1]
|
||||
# removing suffix
|
||||
return bare.split('[')[0]
|
||||
|
||||
def sizeof_field_type(field):
|
||||
return msgtype_size_map[bare_name(field.type)]
|
||||
|
||||
# Function to print a standard ros type
|
||||
def print_field_def(field):
|
||||
type = field.type
|
||||
type_name = field.type
|
||||
# detect embedded types
|
||||
sl_pos = type.find('/')
|
||||
sl_pos = type_name.find('/')
|
||||
type_appendix = ''
|
||||
type_prefix = ''
|
||||
if (sl_pos >= 0):
|
||||
type = type[sl_pos + 1:]
|
||||
type_name = type_name[sl_pos + 1:]
|
||||
type_prefix = 'struct '
|
||||
type_appendix = '_s'
|
||||
|
||||
# detect arrays
|
||||
a_pos = type.find('[')
|
||||
a_pos = type_name.find('[')
|
||||
array_size = ''
|
||||
if (a_pos >= 0):
|
||||
# field is array
|
||||
array_size = type[a_pos:]
|
||||
type = type[:a_pos]
|
||||
array_size = type_name[a_pos:]
|
||||
type_name = type_name[:a_pos]
|
||||
|
||||
if type in type_map:
|
||||
if type_name in type_map:
|
||||
# need to add _t: int8 --> int8_t
|
||||
type_px4 = type_map[type]
|
||||
type_px4 = type_map[type_name]
|
||||
else:
|
||||
raise Exception("Type {0} not supported, add to to template file!".format(type))
|
||||
raise Exception("Type {0} not supported, add to to template file!".format(type_name))
|
||||
|
||||
print('\t%s%s%s %s%s;'%(type_prefix, type_px4, type_appendix, field.name, array_size))
|
||||
|
||||
}
|
||||
def print_parsed_fields():
|
||||
# sort fields
|
||||
sorted_fields = sorted(spec.parsed_fields(), key = sizeof_field_type, reverse=True)
|
||||
# loop over all fields and print the type and name
|
||||
for field in sorted_fields:
|
||||
if (not field.is_header):
|
||||
print_field_def(field)
|
||||
|
||||
}@
|
||||
|
||||
// #pragma pack(push, 1) badly breaks alignment everywhere!
|
||||
#ifdef __cplusplus
|
||||
@#class @(uorb_struct) {
|
||||
struct __EXPORT @(uorb_struct) {
|
||||
@@ -147,31 +181,27 @@ struct __EXPORT @(uorb_struct) {
|
||||
#else
|
||||
struct @(uorb_struct) {
|
||||
#endif
|
||||
@{
|
||||
# loop over all fields and print the type and name
|
||||
for field in spec.parsed_fields():
|
||||
if (not field.is_header):
|
||||
print_field_def(field)
|
||||
}@
|
||||
@# timestamp at the beginning of each topic is required for logger
|
||||
uint64_t timestamp; // required for logger
|
||||
@print_parsed_fields()
|
||||
#ifdef __cplusplus
|
||||
@# Constants again c++-ified
|
||||
@{
|
||||
for constant in spec.constants:
|
||||
type = constant.type
|
||||
if type in type_map:
|
||||
type_name = constant.type
|
||||
if type_name in type_map:
|
||||
# need to add _t: int8 --> int8_t
|
||||
type_px4 = type_map[type]
|
||||
type_px4 = type_map[type_name]
|
||||
else:
|
||||
raise Exception("Type {0} not supported, add to to template file!".format(type))
|
||||
raise Exception("Type {0} not supported, add to to template file!".format(type_name))
|
||||
|
||||
print('\tstatic const %s %s = %s;'%(type_px4, constant.name, int(constant.val)))
|
||||
}
|
||||
#endif
|
||||
};
|
||||
|
||||
/**
|
||||
* @@}
|
||||
*/
|
||||
//#pragma pack(pop)
|
||||
|
||||
/* register this as object request broker structure */
|
||||
ORB_DECLARE(@(topic_name));
|
||||
@[for multi_topic in topics]@
|
||||
ORB_DECLARE(@multi_topic);
|
||||
@[end for]
|
||||
|
||||
@@ -0,0 +1,70 @@
|
||||
@###############################################
|
||||
@#
|
||||
@# EmPy template for generating uORBTopics.cpp file
|
||||
@# for logging purposes
|
||||
@#
|
||||
@###############################################
|
||||
@# Start of Template
|
||||
@#
|
||||
@# Context:
|
||||
@# - msgs (List) list of all msg files
|
||||
@###############################################
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (C) 2013-2015 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.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
#include <uORB/uORBTopics.h>
|
||||
#include <uORB/uORB.h>
|
||||
@{
|
||||
msgs_count = len(msgs)
|
||||
msg_names = [mn.replace(".msg", "") for mn in msgs]
|
||||
}@
|
||||
@[for msg_name in msg_names]@
|
||||
#include <uORB/topics/@(msg_name).h>
|
||||
@[end for]
|
||||
|
||||
const size_t _uorb_topics_count = @(msgs_count);
|
||||
const struct orb_metadata* _uorb_topics_list[_uorb_topics_count] = {
|
||||
@[for idx, msg_name in enumerate(msg_names, 1)]@
|
||||
ORB_ID(@(msg_name))@[if idx != msgs_count],@[end if]
|
||||
@[end for]
|
||||
};
|
||||
|
||||
size_t orb_topics_count()
|
||||
{
|
||||
return _uorb_topics_count;
|
||||
}
|
||||
|
||||
const struct orb_metadata **orb_get_topics()
|
||||
{
|
||||
return _uorb_topics_list;
|
||||
}
|
||||
@@ -1,5 +1,4 @@
|
||||
uint8 NUM_MOTOR_OUTPUTS = 8
|
||||
|
||||
uint64 timestamp # output timestamp in us since system boot
|
||||
uint32 motor_number # number of motor to spin
|
||||
float32 value # output power, range [0..1]
|
||||
|
||||
@@ -1,4 +1,3 @@
|
||||
uint64 timestamp # Timestamp of this position report
|
||||
uint32 ICAO_address # ICAO address
|
||||
float64 lat # Latitude, expressed as degrees
|
||||
float64 lon # Longitude, expressed as degrees
|
||||
|
||||
@@ -1,5 +1,4 @@
|
||||
# This is similar to the mavlink message ATTITUDE, but for onboard use */
|
||||
uint64 timestamp # in microseconds since system start
|
||||
# @warning roll, pitch and yaw have always to be valid, the rotation matrix and quaternion are optional
|
||||
float32 roll # Roll angle (rad, Tait-Bryan, NED)
|
||||
float32 pitch # Pitch angle (rad, Tait-Bryan, NED)
|
||||
|
||||
@@ -8,7 +8,6 @@
|
||||
#
|
||||
###############################################################################################
|
||||
|
||||
uint64 timestamp # in microseconds since system start, is set whenever the writing thread stores new data
|
||||
|
||||
float32 roll_body # body angle in NED frame
|
||||
float32 pitch_body # body angle in NED frame
|
||||
@@ -35,3 +34,6 @@ bool fw_control_yaw # control heading with rudder (used for auto takeoff on
|
||||
bool disable_mc_yaw_control # control yaw for mc (used for vtol weather-vane mode)
|
||||
|
||||
bool apply_flaps
|
||||
|
||||
# WAS vehicle_attitude_setpoint mc_virtual_attitude_setpoint fw_virtual_attitude_setpoint
|
||||
# TOPICS vehicle_attitude_setpoint
|
||||
|
||||
@@ -1,5 +1,4 @@
|
||||
|
||||
uint64 timestamp # in microseconds since system start
|
||||
# is set whenever the writing thread stores new data
|
||||
|
||||
bool flag_armed
|
||||
|
||||
@@ -4,7 +4,6 @@
|
||||
# estimator, which will take more sources of information into account than just GPS,
|
||||
# e.g. control inputs of the vehicle in a Kalman-filter implementation.
|
||||
#
|
||||
uint64 timestamp # Time of this estimate since system start, (microseconds)
|
||||
uint64 time_utc_usec # GPS UTC timestamp, (microseconds)
|
||||
float64 lat # Latitude, (degrees)
|
||||
float64 lon # Longitude, (degrees)
|
||||
|
||||
@@ -1,3 +1,2 @@
|
||||
uint64 timestamp # timestamp of the setpoint
|
||||
bool landed # true if vehicle is currently landed on the ground
|
||||
bool freefall # true if vehicle is currently in free-fall
|
||||
|
||||
@@ -1,6 +1,5 @@
|
||||
# Fused local position in NED.
|
||||
|
||||
uint64 timestamp # Time of this estimate since system start, (microseconds)
|
||||
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
|
||||
|
||||
@@ -1,6 +1,5 @@
|
||||
# Local position setpoint in NED frame
|
||||
|
||||
uint64 timestamp # timestamp of the setpoint
|
||||
float32 x # in meters NED
|
||||
float32 y # in meters NED
|
||||
float32 z # in meters NED
|
||||
|
||||
@@ -8,7 +8,6 @@
|
||||
#
|
||||
###############################################################################################
|
||||
|
||||
uint64 timestamp # in microseconds since system start
|
||||
|
||||
float32 roll # body angular rates in NED frame
|
||||
float32 pitch # body angular rates in NED frame
|
||||
|
||||
@@ -41,7 +41,6 @@ uint8 RC_IN_MODE_GENERATED = 2
|
||||
|
||||
# state machine / state of vehicle.
|
||||
# Encodes the complete system state and is set by the commander app.
|
||||
uint64 timestamp # in microseconds since system start, is set whenever the writing thread stores new data
|
||||
|
||||
uint8 nav_state # set navigation state machine to specified value
|
||||
uint8 arming_state # current arming state
|
||||
|
||||
@@ -5,7 +5,6 @@ uint8 VEHICLE_VTOL_STATE_TRANSITION_TO_MC = 2
|
||||
uint8 VEHICLE_VTOL_STATE_MC = 3
|
||||
uint8 VEHICLE_VTOL_STATE_FW = 4
|
||||
|
||||
uint64 timestamp # Microseconds since system boot
|
||||
bool vtol_in_rw_mode # true: vtol vehicle is in rotating wing mode
|
||||
bool vtol_in_trans_mode
|
||||
bool vtol_transition_failsafe # vtol in transition failsafe mode
|
||||
|
||||
@@ -1,4 +1,3 @@
|
||||
uint64 timestamp # Microseconds since system boot
|
||||
float32 windspeed_north # Wind component in north / X direction
|
||||
float32 windspeed_east # Wind component in east / Y direction
|
||||
float32 covariance_north # Uncertainty - set to zero (no uncertainty) if not estimated
|
||||
|
||||
Reference in New Issue
Block a user