INSTRUCTION stringlengths 1 46.3k | RESPONSE stringlengths 75 80.2k |
|---|---|
The filtered global position (e.g. fused GPS and accelerometers). The
position is in GPS-frame (right-handed, Z-up). It
is designed as scaled integer message since the
resolution of float is not sufficient.
time_boot_ms : Timestamp (milliseco... | def global_position_int_encode(self, time_boot_ms, lat, lon, alt, relative_alt, vx, vy, vz, hdg):
'''
The filtered global position (e.g. fused GPS and accelerometers). The
position is in GPS-frame (right-handed, Z-up). It
is designed as scaled integer mess... |
The filtered global position (e.g. fused GPS and accelerometers). The
position is in GPS-frame (right-handed, Z-up). It
is designed as scaled integer message since the
resolution of float is not sufficient.
time_boot_ms : Timestamp (milliseco... | def global_position_int_send(self, time_boot_ms, lat, lon, alt, relative_alt, vx, vy, vz, hdg, force_mavlink1=False):
'''
The filtered global position (e.g. fused GPS and accelerometers). The
position is in GPS-frame (right-handed, Z-up). It
is designed as... |
The scaled values of the RC channels received. (-100%) -10000, (0%) 0,
(100%) 10000. Channels that are inactive should be set
to UINT16_MAX.
time_boot_ms : Timestamp (milliseconds since system boot) (uint32_t)
port : Serv... | def rc_channels_scaled_encode(self, time_boot_ms, port, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi):
'''
The scaled values of the RC channels received. (-100%) -10000, (0%) 0,
(100%) 10000. Channels... |
The scaled values of the RC channels received. (-100%) -10000, (0%) 0,
(100%) 10000. Channels that are inactive should be set
to UINT16_MAX.
time_boot_ms : Timestamp (milliseconds since system boot) (uint32_t)
port : Serv... | def rc_channels_scaled_send(self, time_boot_ms, port, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi, force_mavlink1=False):
'''
The scaled values of the RC channels received. (-100%) -10000, (0%) 0,
(1... |
The RAW values of the RC channels received. The standard PPM
modulation is as follows: 1000 microseconds: 0%, 2000
microseconds: 100%. Individual receivers/transmitters
might violate this specification.
time_boot_ms : Timestamp (milliseconds ... | def rc_channels_raw_encode(self, time_boot_ms, port, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi):
'''
The RAW values of the RC channels received. The standard PPM
modulation is as follows: 1000 microseconds: 0%, 2000
... |
The RAW values of the RC channels received. The standard PPM
modulation is as follows: 1000 microseconds: 0%, 2000
microseconds: 100%. Individual receivers/transmitters
might violate this specification.
time_boot_ms : Timestamp (milliseconds ... | def rc_channels_raw_send(self, time_boot_ms, port, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi, force_mavlink1=False):
'''
The RAW values of the RC channels received. The standard PPM
modulation is as follows: 1000 microsec... |
The RAW values of the servo outputs (for RC input from the remote, use
the RC_CHANNELS messages). The standard PPM modulation
is as follows: 1000 microseconds: 0%, 2000
microseconds: 100%.
time_usec : Timestamp (microseconds since system b... | def servo_output_raw_encode(self, time_usec, port, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw):
'''
The RAW values of the servo outputs (for RC input from the remote, use
the RC_CHANNELS messages). The standard PPM modul... |
The RAW values of the servo outputs (for RC input from the remote, use
the RC_CHANNELS messages). The standard PPM modulation
is as follows: 1000 microseconds: 0%, 2000
microseconds: 100%.
time_usec : Timestamp (microseconds since system b... | def servo_output_raw_send(self, time_usec, port, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw, force_mavlink1=False):
'''
The RAW values of the servo outputs (for RC input from the remote, use
the RC_CHANNELS messages). Th... |
Request a partial list of mission items from the system/component.
http://qgroundcontrol.org/mavlink/waypoint_protocol.
If start and end index are the same, just send one
waypoint.
target_system : System ID (uint8_t)
target_com... | def mission_request_partial_list_encode(self, target_system, target_component, start_index, end_index):
'''
Request a partial list of mission items from the system/component.
http://qgroundcontrol.org/mavlink/waypoint_protocol.
If start and end index are t... |
Request a partial list of mission items from the system/component.
http://qgroundcontrol.org/mavlink/waypoint_protocol.
If start and end index are the same, just send one
waypoint.
target_system : System ID (uint8_t)
target_com... | def mission_request_partial_list_send(self, target_system, target_component, start_index, end_index, force_mavlink1=False):
'''
Request a partial list of mission items from the system/component.
http://qgroundcontrol.org/mavlink/waypoint_protocol.
If start... |
This message is sent to the MAV to write a partial list. If start
index == end index, only one item will be transmitted
/ updated. If the start index is NOT 0 and above the
current list size, this request should be REJECTED!
target_system : Sy... | def mission_write_partial_list_encode(self, target_system, target_component, start_index, end_index):
'''
This message is sent to the MAV to write a partial list. If start
index == end index, only one item will be transmitted
/ updated. If the start index ... |
This message is sent to the MAV to write a partial list. If start
index == end index, only one item will be transmitted
/ updated. If the start index is NOT 0 and above the
current list size, this request should be REJECTED!
target_system : Sy... | def mission_write_partial_list_send(self, target_system, target_component, start_index, end_index, force_mavlink1=False):
'''
This message is sent to the MAV to write a partial list. If start
index == end index, only one item will be transmitted
/ updated.... |
Message encoding a mission item. This message is emitted to announce
the presence of a mission item and to set a mission
item on the system. The mission item can be either in
x, y, z meters (type: LOCAL) or x:lat, y:lon,
z:altitude. Local frame is Z-down, ... | def mission_item_encode(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
'''
Message encoding a mission item. This message is emitted to announce
the presence of a mission item and to set a missio... |
Request the information of the mission item with the sequence number
seq. The response of the system to this message should
be a MISSION_ITEM message.
http://qgroundcontrol.org/mavlink/waypoint_protocol
target_system : System ID (uint8_t)
... | def mission_request_send(self, target_system, target_component, seq, force_mavlink1=False):
'''
Request the information of the mission item with the sequence number
seq. The response of the system to this message should
be a MISSION_ITEM message.
... |
Set the mission item with sequence number seq as current item. This
means that the MAV will continue to this mission item
on the shortest path (not following the mission items
in-between).
target_system : System ID (uint8_t)
ta... | def mission_set_current_send(self, target_system, target_component, seq, force_mavlink1=False):
'''
Set the mission item with sequence number seq as current item. This
means that the MAV will continue to this mission item
on the shortest path (not followin... |
Request the overall list of mission items from the system/component.
target_system : System ID (uint8_t)
target_component : Component ID (uint8_t) | def mission_request_list_send(self, target_system, target_component, force_mavlink1=False):
'''
Request the overall list of mission items from the system/component.
target_system : System ID (uint8_t)
target_component : Component ID (... |
Message that announces the sequence number of the current active
mission item. The MAV will fly towards this mission
item.
seq : Sequence (uint16_t) | def mission_current_send(self, seq, force_mavlink1=False):
'''
Message that announces the sequence number of the current active
mission item. The MAV will fly towards this mission
item.
seq : Sequence (uint16_t)
... |
This message is emitted as response to MISSION_REQUEST_LIST by the MAV
and to initiate a write transaction. The GCS can then
request the individual mission item based on the
knowledge of the total number of MISSIONs.
target_system : System ID ... | def mission_count_send(self, target_system, target_component, count, force_mavlink1=False):
'''
This message is emitted as response to MISSION_REQUEST_LIST by the MAV
and to initiate a write transaction. The GCS can then
request the individual mission item... |
Delete all mission items at once.
target_system : System ID (uint8_t)
target_component : Component ID (uint8_t) | def mission_clear_all_send(self, target_system, target_component, force_mavlink1=False):
'''
Delete all mission items at once.
target_system : System ID (uint8_t)
target_component : Component ID (uint8_t)
'''
... |
A certain mission item has been reached. The system will either hold
this position (or circle on the orbit) or (if the
autocontinue on the WP was set) continue to the next
MISSION.
seq : Sequence (uint16_t) | def mission_item_reached_send(self, seq, force_mavlink1=False):
'''
A certain mission item has been reached. The system will either hold
this position (or circle on the orbit) or (if the
autocontinue on the WP was set) continue to the next
... |
Ack message during MISSION handling. The type field states if this
message is a positive ack (type=0) or if an error
happened (type=non-zero).
target_system : System ID (uint8_t)
target_component : Component ID (uint8_t)
... | def mission_ack_send(self, target_system, target_component, type, force_mavlink1=False):
'''
Ack message during MISSION handling. The type field states if this
message is a positive ack (type=0) or if an error
happened (type=non-zero).
tar... |
As local waypoints exist, the global MISSION reference allows to
transform between the local coordinate frame and the
global (GPS) coordinate frame. This can be necessary
when e.g. in- and outdoor settings are connected and
the MAV should move from in- to ... | def set_gps_global_origin_encode(self, target_system, latitude, longitude, altitude):
'''
As local waypoints exist, the global MISSION reference allows to
transform between the local coordinate frame and the
global (GPS) coordinate frame. This can be neces... |
As local waypoints exist, the global MISSION reference allows to
transform between the local coordinate frame and the
global (GPS) coordinate frame. This can be necessary
when e.g. in- and outdoor settings are connected and
the MAV should move from in- to ... | def set_gps_global_origin_send(self, target_system, latitude, longitude, altitude, force_mavlink1=False):
'''
As local waypoints exist, the global MISSION reference allows to
transform between the local coordinate frame and the
global (GPS) coordinate fram... |
Once the MAV sets a new GPS-Local correspondence, this message
announces the origin (0,0,0) position
latitude : Latitude (WGS84), in degrees * 1E7 (int32_t)
longitude : Longitude (WGS84), in degrees * 1E7 (int32_t)
altitud... | def gps_global_origin_send(self, latitude, longitude, altitude, force_mavlink1=False):
'''
Once the MAV sets a new GPS-Local correspondence, this message
announces the origin (0,0,0) position
latitude : Latitude (WGS84), in degrees * 1E7 ... |
Bind a RC channel to a parameter. The parameter should change accoding
to the RC channel value.
target_system : System ID (uint8_t)
target_component : Component ID (uint8_t)
param_id : Onboard parameter id, terminated... | def param_map_rc_encode(self, target_system, target_component, param_id, param_index, parameter_rc_channel_index, param_value0, scale, param_value_min, param_value_max):
'''
Bind a RC channel to a parameter. The parameter should change accoding
to the RC channel value.
... |
Bind a RC channel to a parameter. The parameter should change accoding
to the RC channel value.
target_system : System ID (uint8_t)
target_component : Component ID (uint8_t)
param_id : Onboard parameter id, terminated... | def param_map_rc_send(self, target_system, target_component, param_id, param_index, parameter_rc_channel_index, param_value0, scale, param_value_min, param_value_max, force_mavlink1=False):
'''
Bind a RC channel to a parameter. The parameter should change accoding
to the ... |
Request the information of the mission item with the sequence number
seq. The response of the system to this message should
be a MISSION_ITEM_INT message.
http://qgroundcontrol.org/mavlink/waypoint_protocol
target_system : System ID (uint8_t)
... | def mission_request_int_send(self, target_system, target_component, seq, force_mavlink1=False):
'''
Request the information of the mission item with the sequence number
seq. The response of the system to this message should
be a MISSION_ITEM_INT message.
... |
Set a safety zone (volume), which is defined by two corners of a cube.
This message can be used to tell the MAV which
setpoints/MISSIONs to accept and which to reject.
Safety areas are often enforced by national or
competition regulations.
... | def safety_set_allowed_area_encode(self, target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z):
'''
Set a safety zone (volume), which is defined by two corners of a cube.
This message can be used to tell the MAV which
setpoints/MISSIONs to ... |
Set a safety zone (volume), which is defined by two corners of a cube.
This message can be used to tell the MAV which
setpoints/MISSIONs to accept and which to reject.
Safety areas are often enforced by national or
competition regulations.
... | def safety_set_allowed_area_send(self, target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z, force_mavlink1=False):
'''
Set a safety zone (volume), which is defined by two corners of a cube.
This message can be used to tell the MAV which
se... |
Read out the safety zone the MAV currently assumes.
frame : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
p1x : x position... | def safety_allowed_area_encode(self, frame, p1x, p1y, p1z, p2x, p2y, p2z):
'''
Read out the safety zone the MAV currently assumes.
frame : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with ... |
Read out the safety zone the MAV currently assumes.
frame : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
p1x : x position... | def safety_allowed_area_send(self, frame, p1x, p1y, p1z, p2x, p2y, p2z, force_mavlink1=False):
'''
Read out the safety zone the MAV currently assumes.
frame : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS... |
The attitude in the aeronautical frame (right-handed, Z-down, X-front,
Y-right), expressed as quaternion. Quaternion order is
w, x, y, z and a zero rotation would be expressed as
(1 0 0 0).
time_boot_ms : Timestamp (milliseconds since system ... | def attitude_quaternion_cov_encode(self, time_boot_ms, q, rollspeed, pitchspeed, yawspeed, covariance):
'''
The attitude in the aeronautical frame (right-handed, Z-down, X-front,
Y-right), expressed as quaternion. Quaternion order is
w, x, y, z and a zero ... |
The attitude in the aeronautical frame (right-handed, Z-down, X-front,
Y-right), expressed as quaternion. Quaternion order is
w, x, y, z and a zero rotation would be expressed as
(1 0 0 0).
time_boot_ms : Timestamp (milliseconds since system ... | def attitude_quaternion_cov_send(self, time_boot_ms, q, rollspeed, pitchspeed, yawspeed, covariance, force_mavlink1=False):
'''
The attitude in the aeronautical frame (right-handed, Z-down, X-front,
Y-right), expressed as quaternion. Quaternion order is
w,... |
The state of the fixed wing navigation and position controller.
nav_roll : Current desired roll in degrees (float)
nav_pitch : Current desired pitch in degrees (float)
nav_bearing : Current desired heading in degrees (int16_... | def nav_controller_output_encode(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error):
'''
The state of the fixed wing navigation and position controller.
nav_roll : Current desired roll in degrees (float)... |
The state of the fixed wing navigation and position controller.
nav_roll : Current desired roll in degrees (float)
nav_pitch : Current desired pitch in degrees (float)
nav_bearing : Current desired heading in degrees (int16_... | def nav_controller_output_send(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error, force_mavlink1=False):
'''
The state of the fixed wing navigation and position controller.
nav_roll : Current desired rol... |
The filtered global position (e.g. fused GPS and accelerometers). The
position is in GPS-frame (right-handed, Z-up). It is
designed as scaled integer message since the
resolution of float is not sufficient. NOTE: This
message is intended for onboard netwo... | def global_position_int_cov_encode(self, time_boot_ms, time_utc, estimator_type, lat, lon, alt, relative_alt, vx, vy, vz, covariance):
'''
The filtered global position (e.g. fused GPS and accelerometers). The
position is in GPS-frame (right-handed, Z-up). It is
... |
The filtered global position (e.g. fused GPS and accelerometers). The
position is in GPS-frame (right-handed, Z-up). It is
designed as scaled integer message since the
resolution of float is not sufficient. NOTE: This
message is intended for onboard netwo... | def global_position_int_cov_send(self, time_boot_ms, time_utc, estimator_type, lat, lon, alt, relative_alt, vx, vy, vz, covariance, force_mavlink1=False):
'''
The filtered global position (e.g. fused GPS and accelerometers). The
position is in GPS-frame (right-handed, Z-u... |
The filtered local position (e.g. fused computer vision and
accelerometers). Coordinate frame is right-handed,
Z-axis down (aeronautical frame, NED / north-east-down
convention)
time_boot_ms : Timestamp (milliseconds since system boot). 0 for... | def local_position_ned_cov_encode(self, time_boot_ms, time_utc, estimator_type, x, y, z, vx, vy, vz, ax, ay, az, covariance):
'''
The filtered local position (e.g. fused computer vision and
accelerometers). Coordinate frame is right-handed,
Z-axis down (ae... |
The filtered local position (e.g. fused computer vision and
accelerometers). Coordinate frame is right-handed,
Z-axis down (aeronautical frame, NED / north-east-down
convention)
time_boot_ms : Timestamp (milliseconds since system boot). 0 for... | def local_position_ned_cov_send(self, time_boot_ms, time_utc, estimator_type, x, y, z, vx, vy, vz, ax, ay, az, covariance, force_mavlink1=False):
'''
The filtered local position (e.g. fused computer vision and
accelerometers). Coordinate frame is right-handed,
... |
The PPM values of the RC channels received. The standard PPM
modulation is as follows: 1000 microseconds: 0%, 2000
microseconds: 100%. Individual receivers/transmitters
might violate this specification.
time_boot_ms : Timestamp (milliseconds ... | def rc_channels_encode(self, time_boot_ms, chancount, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, chan13_raw, chan14_raw, chan15_raw, chan16_raw, chan17_raw, chan18_raw, rssi):
'''
The PPM values o... |
THIS INTERFACE IS DEPRECATED. USE SET_MESSAGE_INTERVAL INSTEAD.
target_system : The target requested to send the message stream. (uint8_t)
target_component : The target requested to send the message stream. (uint8_t)
req_stream_id : The I... | def request_data_stream_encode(self, target_system, target_component, req_stream_id, req_message_rate, start_stop):
'''
THIS INTERFACE IS DEPRECATED. USE SET_MESSAGE_INTERVAL INSTEAD.
target_system : The target requested to send the message stream. (uint8_t)
... |
THIS INTERFACE IS DEPRECATED. USE SET_MESSAGE_INTERVAL INSTEAD.
target_system : The target requested to send the message stream. (uint8_t)
target_component : The target requested to send the message stream. (uint8_t)
req_stream_id : The I... | def request_data_stream_send(self, target_system, target_component, req_stream_id, req_message_rate, start_stop, force_mavlink1=False):
'''
THIS INTERFACE IS DEPRECATED. USE SET_MESSAGE_INTERVAL INSTEAD.
target_system : The target requested to send the messag... |
THIS INTERFACE IS DEPRECATED. USE MESSAGE_INTERVAL INSTEAD.
stream_id : The ID of the requested data stream (uint8_t)
message_rate : The message rate (uint16_t)
on_off : 1 stream is enabled, 0 stream is stopped. (uint8_t) | def data_stream_send(self, stream_id, message_rate, on_off, force_mavlink1=False):
'''
THIS INTERFACE IS DEPRECATED. USE MESSAGE_INTERVAL INSTEAD.
stream_id : The ID of the requested data stream (uint8_t)
message_rate : The me... |
This message provides an API for manually controlling the vehicle
using standard joystick axes nomenclature, along with
a joystick-like input device. Unused axes can be
disabled an buttons are also transmit as boolean
values of their
targe... | def manual_control_encode(self, target, x, y, z, r, buttons):
'''
This message provides an API for manually controlling the vehicle
using standard joystick axes nomenclature, along with
a joystick-like input device. Unused axes can be
disab... |
The RAW values of the RC channels sent to the MAV to override info
received from the RC radio. A value of UINT16_MAX
means no change to that channel. A value of 0 means
control of that channel should be released back to the
RC radio. The standard PPM modul... | def rc_channels_override_encode(self, target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw):
'''
The RAW values of the RC channels sent to the MAV to override info
received from the RC radio. A value of UI... |
This message provides an API for manually controlling the vehicle
using standard joystick axes nomenclature, along with
a joystick-like input device. Unused axes can be
disabled an buttons are also transmit as boolean
values of their
targe... | def manual_control_send(self, target, x, y, z, r, buttons, force_mavlink1=False):
'''
This message provides an API for manually controlling the vehicle
using standard joystick axes nomenclature, along with
a joystick-like input device. Unused axes can be
... |
The RAW values of the RC channels sent to the MAV to override info
received from the RC radio. A value of UINT16_MAX
means no change to that channel. A value of 0 means
control of that channel should be released back to the
RC radio. The standard PPM modul... | def rc_channels_override_send(self, target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, force_mavlink1=False):
'''
The RAW values of the RC channels sent to the MAV to override info
received from the RC ... |
Message encoding a mission item. This message is emitted to announce
the presence of a mission item and to set a mission
item on the system. The mission item can be either in
x, y, z meters (type: LOCAL) or x:lat, y:lon,
z:altitude. Local frame is Z-down, ... | def mission_item_int_encode(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
'''
Message encoding a mission item. This message is emitted to announce
the presence of a mission item and to set a mi... |
Message encoding a mission item. This message is emitted to announce
the presence of a mission item and to set a mission
item on the system. The mission item can be either in
x, y, z meters (type: LOCAL) or x:lat, y:lon,
z:altitude. Local frame is Z-down, ... | def mission_item_int_send(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z, force_mavlink1=False):
'''
Message encoding a mission item. This message is emitted to announce
the presence of a mission ... |
Metrics typically displayed on a HUD for fixed wing aircraft
airspeed : Current airspeed in m/s (float)
groundspeed : Current ground speed in m/s (float)
heading : Current heading in degrees, in compass units (0..360, 0=no... | def vfr_hud_encode(self, airspeed, groundspeed, heading, throttle, alt, climb):
'''
Metrics typically displayed on a HUD for fixed wing aircraft
airspeed : Current airspeed in m/s (float)
groundspeed : Current ground speed i... |
Metrics typically displayed on a HUD for fixed wing aircraft
airspeed : Current airspeed in m/s (float)
groundspeed : Current ground speed in m/s (float)
heading : Current heading in degrees, in compass units (0..360, 0=no... | def vfr_hud_send(self, airspeed, groundspeed, heading, throttle, alt, climb, force_mavlink1=False):
'''
Metrics typically displayed on a HUD for fixed wing aircraft
airspeed : Current airspeed in m/s (float)
groundspeed : Cu... |
Message encoding a command with parameters as scaled integers. Scaling
depends on the actual command value.
target_system : System ID (uint8_t)
target_component : Component ID (uint8_t)
frame : The coordinate syste... | def command_int_encode(self, target_system, target_component, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
'''
Message encoding a command with parameters as scaled integers. Scaling
depends on the actual command value.
... |
Message encoding a command with parameters as scaled integers. Scaling
depends on the actual command value.
target_system : System ID (uint8_t)
target_component : Component ID (uint8_t)
frame : The coordinate syste... | def command_int_send(self, target_system, target_component, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z, force_mavlink1=False):
'''
Message encoding a command with parameters as scaled integers. Scaling
depends on the actual command valu... |
Send a command with up to seven parameters to the MAV
target_system : System which should execute the command (uint8_t)
target_component : Component which should execute the command, 0 for all components (uint8_t)
command : Command ... | def command_long_encode(self, target_system, target_component, command, confirmation, param1, param2, param3, param4, param5, param6, param7):
'''
Send a command with up to seven parameters to the MAV
target_system : System which should execute the command (u... |
Send a command with up to seven parameters to the MAV
target_system : System which should execute the command (uint8_t)
target_component : Component which should execute the command, 0 for all components (uint8_t)
command : Command ... | def command_long_send(self, target_system, target_component, command, confirmation, param1, param2, param3, param4, param5, param6, param7, force_mavlink1=False):
'''
Send a command with up to seven parameters to the MAV
target_system : System which should ex... |
Report status of a command. Includes feedback wether the command was
executed.
command : Command ID, as defined by MAV_CMD enum. (uint16_t)
result : See MAV_RESULT enum (uint8_t) | def command_ack_send(self, command, result, force_mavlink1=False):
'''
Report status of a command. Includes feedback wether the command was
executed.
command : Command ID, as defined by MAV_CMD enum. (uint16_t)
result ... |
Setpoint in roll, pitch, yaw and thrust from the operator
time_boot_ms : Timestamp in milliseconds since system boot (uint32_t)
roll : Desired roll rate in radians per second (float)
pitch : Desired pitch rate in radi... | def manual_setpoint_encode(self, time_boot_ms, roll, pitch, yaw, thrust, mode_switch, manual_override_switch):
'''
Setpoint in roll, pitch, yaw and thrust from the operator
time_boot_ms : Timestamp in milliseconds since system boot (uint32_t)
... |
Setpoint in roll, pitch, yaw and thrust from the operator
time_boot_ms : Timestamp in milliseconds since system boot (uint32_t)
roll : Desired roll rate in radians per second (float)
pitch : Desired pitch rate in radi... | def manual_setpoint_send(self, time_boot_ms, roll, pitch, yaw, thrust, mode_switch, manual_override_switch, force_mavlink1=False):
'''
Setpoint in roll, pitch, yaw and thrust from the operator
time_boot_ms : Timestamp in milliseconds since system boot (uint3... |
Sets a desired vehicle attitude. Used by an external controller to
command the vehicle (manual controller or other
system).
time_boot_ms : Timestamp in milliseconds since system boot (uint32_t)
target_system : System ID (uint8_t)
... | def set_attitude_target_encode(self, time_boot_ms, target_system, target_component, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust):
'''
Sets a desired vehicle attitude. Used by an external controller to
command the vehicle (manual controller or othe... |
Sets a desired vehicle attitude. Used by an external controller to
command the vehicle (manual controller or other
system).
time_boot_ms : Timestamp in milliseconds since system boot (uint32_t)
target_system : System ID (uint8_t)
... | def set_attitude_target_send(self, time_boot_ms, target_system, target_component, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust, force_mavlink1=False):
'''
Sets a desired vehicle attitude. Used by an external controller to
command the vehicle (manua... |
Reports the current commanded attitude of the vehicle as specified by
the autopilot. This should match the commands sent in
a SET_ATTITUDE_TARGET message if the vehicle is being
controlled this way.
time_boot_ms : Timestamp in milliseconds si... | def attitude_target_encode(self, time_boot_ms, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust):
'''
Reports the current commanded attitude of the vehicle as specified by
the autopilot. This should match the commands sent in
a SET_ATTI... |
Reports the current commanded attitude of the vehicle as specified by
the autopilot. This should match the commands sent in
a SET_ATTITUDE_TARGET message if the vehicle is being
controlled this way.
time_boot_ms : Timestamp in milliseconds si... | def attitude_target_send(self, time_boot_ms, type_mask, q, body_roll_rate, body_pitch_rate, body_yaw_rate, thrust, force_mavlink1=False):
'''
Reports the current commanded attitude of the vehicle as specified by
the autopilot. This should match the commands sent in
... |
Sets a desired vehicle position in a local north-east-down coordinate
frame. Used by an external controller to command the
vehicle (manual controller or other system).
time_boot_ms : Timestamp in milliseconds since system boot (uint32_t)
targ... | def set_position_target_local_ned_encode(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
'''
Sets a desired vehicle position in a local north-east-down coordinate
frame. Used by an exter... |
Sets a desired vehicle position in a local north-east-down coordinate
frame. Used by an external controller to command the
vehicle (manual controller or other system).
time_boot_ms : Timestamp in milliseconds since system boot (uint32_t)
targ... | def set_position_target_local_ned_send(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate, force_mavlink1=False):
'''
Sets a desired vehicle position in a local north-east-down coordinate
fra... |
Reports the current commanded vehicle position, velocity, and
acceleration as specified by the autopilot. This
should match the commands sent in
SET_POSITION_TARGET_LOCAL_NED if the vehicle is being
controlled this way.
time_boot_ms ... | def position_target_local_ned_encode(self, time_boot_ms, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
'''
Reports the current commanded vehicle position, velocity, and
acceleration as specified by the autopilot. This
sho... |
Reports the current commanded vehicle position, velocity, and
acceleration as specified by the autopilot. This
should match the commands sent in
SET_POSITION_TARGET_LOCAL_NED if the vehicle is being
controlled this way.
time_boot_ms ... | def position_target_local_ned_send(self, time_boot_ms, coordinate_frame, type_mask, x, y, z, vx, vy, vz, afx, afy, afz, yaw, yaw_rate, force_mavlink1=False):
'''
Reports the current commanded vehicle position, velocity, and
acceleration as specified by the autopilot. This... |
Sets a desired vehicle position, velocity, and/or acceleration in a
global coordinate system (WGS84). Used by an external
controller to command the vehicle (manual controller
or other system).
time_boot_ms : Timestamp in milliseconds since sy... | def set_position_target_global_int_encode(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
'''
Sets a desired vehicle position, velocity, and/or acceleration in a
global coo... |
Sets a desired vehicle position, velocity, and/or acceleration in a
global coordinate system (WGS84). Used by an external
controller to command the vehicle (manual controller
or other system).
time_boot_ms : Timestamp in milliseconds since sy... | def set_position_target_global_int_send(self, time_boot_ms, target_system, target_component, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate, force_mavlink1=False):
'''
Sets a desired vehicle position, velocity, and/or acceleration in a
... |
Reports the current commanded vehicle position, velocity, and
acceleration as specified by the autopilot. This
should match the commands sent in
SET_POSITION_TARGET_GLOBAL_INT if the vehicle is being
controlled this way.
time_boot_ms ... | def position_target_global_int_encode(self, time_boot_ms, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate):
'''
Reports the current commanded vehicle position, velocity, and
acceleration as specified by the autopilot. This
... |
Reports the current commanded vehicle position, velocity, and
acceleration as specified by the autopilot. This
should match the commands sent in
SET_POSITION_TARGET_GLOBAL_INT if the vehicle is being
controlled this way.
time_boot_ms ... | def position_target_global_int_send(self, time_boot_ms, coordinate_frame, type_mask, lat_int, lon_int, alt, vx, vy, vz, afx, afy, afz, yaw, yaw_rate, force_mavlink1=False):
'''
Reports the current commanded vehicle position, velocity, and
acceleration as specified by the ... |
The offset in X, Y, Z and yaw between the LOCAL_POSITION_NED messages
of MAV X and the global coordinate frame in NED
coordinates. Coordinate frame is right-handed, Z-axis
down (aeronautical frame, NED / north-east-down
convention)
time_bo... | def local_position_ned_system_global_offset_encode(self, time_boot_ms, x, y, z, roll, pitch, yaw):
'''
The offset in X, Y, Z and yaw between the LOCAL_POSITION_NED messages
of MAV X and the global coordinate frame in NED
coordinates. Coordinate frame is ri... |
The offset in X, Y, Z and yaw between the LOCAL_POSITION_NED messages
of MAV X and the global coordinate frame in NED
coordinates. Coordinate frame is right-handed, Z-axis
down (aeronautical frame, NED / north-east-down
convention)
time_bo... | def local_position_ned_system_global_offset_send(self, time_boot_ms, x, y, z, roll, pitch, yaw, force_mavlink1=False):
'''
The offset in X, Y, Z and yaw between the LOCAL_POSITION_NED messages
of MAV X and the global coordinate frame in NED
coordinates. Co... |
DEPRECATED PACKET! Suffers from missing airspeed fields and
singularities due to Euler angles. Please use
HIL_STATE_QUATERNION instead. Sent from simulation to
autopilot. This packet is useful for high throughput
applications such as hardware in the loop s... | def hil_state_encode(self, time_usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc):
'''
DEPRECATED PACKET! Suffers from missing airspeed fields and
singularities due to Euler angles. Please use
HIL_STATE_Q... |
DEPRECATED PACKET! Suffers from missing airspeed fields and
singularities due to Euler angles. Please use
HIL_STATE_QUATERNION instead. Sent from simulation to
autopilot. This packet is useful for high throughput
applications such as hardware in the loop s... | def hil_state_send(self, time_usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc, force_mavlink1=False):
'''
DEPRECATED PACKET! Suffers from missing airspeed fields and
singularities due to Euler angles. Please use
... |
Sent from autopilot to simulation. Hardware in the loop control
outputs
time_usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
roll_ailerons : Control output -1 .. 1 (float)
pitch_ele... | def hil_controls_encode(self, time_usec, roll_ailerons, pitch_elevator, yaw_rudder, throttle, aux1, aux2, aux3, aux4, mode, nav_mode):
'''
Sent from autopilot to simulation. Hardware in the loop control
outputs
time_usec : Timestamp (micro... |
Sent from autopilot to simulation. Hardware in the loop control
outputs
time_usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
roll_ailerons : Control output -1 .. 1 (float)
pitch_ele... | def hil_controls_send(self, time_usec, roll_ailerons, pitch_elevator, yaw_rudder, throttle, aux1, aux2, aux3, aux4, mode, nav_mode, force_mavlink1=False):
'''
Sent from autopilot to simulation. Hardware in the loop control
outputs
time_usec ... |
Sent from simulation to autopilot. The RAW values of the RC channels
received. The standard PPM modulation is as follows:
1000 microseconds: 0%, 2000 microseconds: 100%.
Individual receivers/transmitters might violate this
specification.
t... | def hil_rc_inputs_raw_encode(self, time_usec, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, rssi):
'''
Sent from simulation to autopilot. The RAW values of the RC channels
received. T... |
Sent from simulation to autopilot. The RAW values of the RC channels
received. The standard PPM modulation is as follows:
1000 microseconds: 0%, 2000 microseconds: 100%.
Individual receivers/transmitters might violate this
specification.
t... | def hil_rc_inputs_raw_send(self, time_usec, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, chan9_raw, chan10_raw, chan11_raw, chan12_raw, rssi, force_mavlink1=False):
'''
Sent from simulation to autopilot. The RAW values of the RC channels
... |
Sent from autopilot to simulation. Hardware in the loop control
outputs (replacement for HIL_CONTROLS)
time_usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
controls : Control outputs -1 .. 1. ... | def hil_actuator_controls_encode(self, time_usec, controls, mode, flags):
'''
Sent from autopilot to simulation. Hardware in the loop control
outputs (replacement for HIL_CONTROLS)
time_usec : Timestamp (microseconds since UNIX epoch or mi... |
Sent from autopilot to simulation. Hardware in the loop control
outputs (replacement for HIL_CONTROLS)
time_usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
controls : Control outputs -1 .. 1. ... | def hil_actuator_controls_send(self, time_usec, controls, mode, flags, force_mavlink1=False):
'''
Sent from autopilot to simulation. Hardware in the loop control
outputs (replacement for HIL_CONTROLS)
time_usec : Timestamp (microseconds si... |
Optical flow from a flow sensor (e.g. optical mouse sensor)
time_usec : Timestamp (UNIX) (uint64_t)
sensor_id : Sensor ID (uint8_t)
flow_x : Flow in pixels * 10 in x-sensor direction (dezi-pixels) (int16_t)
... | def optical_flow_encode(self, time_usec, sensor_id, flow_x, flow_y, flow_comp_m_x, flow_comp_m_y, quality, ground_distance):
'''
Optical flow from a flow sensor (e.g. optical mouse sensor)
time_usec : Timestamp (UNIX) (uint64_t)
sensor_id ... |
Optical flow from a flow sensor (e.g. optical mouse sensor)
time_usec : Timestamp (UNIX) (uint64_t)
sensor_id : Sensor ID (uint8_t)
flow_x : Flow in pixels * 10 in x-sensor direction (dezi-pixels) (int16_t)
... | def optical_flow_send(self, time_usec, sensor_id, flow_x, flow_y, flow_comp_m_x, flow_comp_m_y, quality, ground_distance, force_mavlink1=False):
'''
Optical flow from a flow sensor (e.g. optical mouse sensor)
time_usec : Timestamp (UNIX) (uint64_t)
... |
The IMU readings in SI units in NED body frame
time_usec : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
xacc : X acceleration (m/s^2) (float)
yacc : Y acceleration (m/s^2) (float)
... | def highres_imu_encode(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated):
'''
The IMU readings in SI units in NED body frame
time_usec : Timestamp (microsecond... |
The IMU readings in SI units in NED body frame
time_usec : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
xacc : X acceleration (m/s^2) (float)
yacc : Y acceleration (m/s^2) (float)
... | def highres_imu_send(self, time_usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature, fields_updated, force_mavlink1=False):
'''
The IMU readings in SI units in NED body frame
time_usec : Ti... |
Optical flow from an angular rate flow sensor (e.g. PX4FLOW or mouse
sensor)
time_usec : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
sensor_id : Sensor ID (uint8_t)
integration_time_us ... | def optical_flow_rad_encode(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance):
'''
Optical flow from an angular rate flow sensor (e.g. PX4FLOW or mouse... |
Optical flow from an angular rate flow sensor (e.g. PX4FLOW or mouse
sensor)
time_usec : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
sensor_id : Sensor ID (uint8_t)
integration_time_us ... | def optical_flow_rad_send(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance, force_mavlink1=False):
'''
Optical flow from an angular rate flow sensor (e... |
Status of simulation environment, if used
q1 : True attitude quaternion component 1, w (1 in null-rotation) (float)
q2 : True attitude quaternion component 2, x (0 in null-rotation) (float)
q3 : True at... | def sim_state_encode(self, q1, q2, q3, q4, roll, pitch, yaw, xacc, yacc, zacc, xgyro, ygyro, zgyro, lat, lon, alt, std_dev_horz, std_dev_vert, vn, ve, vd):
'''
Status of simulation environment, if used
q1 : True attitude quaternion component 1, w (... |
Status generated by radio and injected into MAVLink stream.
rssi : Local signal strength (uint8_t)
remrssi : Remote signal strength (uint8_t)
txbuf : Remaining free buffer space in percent. (uint8_t)
... | def radio_status_encode(self, rssi, remrssi, txbuf, noise, remnoise, rxerrors, fixed):
'''
Status generated by radio and injected into MAVLink stream.
rssi : Local signal strength (uint8_t)
remrssi : Remote signal st... |
Status generated by radio and injected into MAVLink stream.
rssi : Local signal strength (uint8_t)
remrssi : Remote signal strength (uint8_t)
txbuf : Remaining free buffer space in percent. (uint8_t)
... | def radio_status_send(self, rssi, remrssi, txbuf, noise, remnoise, rxerrors, fixed, force_mavlink1=False):
'''
Status generated by radio and injected into MAVLink stream.
rssi : Local signal strength (uint8_t)
remrssi ... |
File transfer message
target_network : Network ID (0 for broadcast) (uint8_t)
target_system : System ID (0 for broadcast) (uint8_t)
target_component : Component ID (0 for broadcast) (uint8_t)
payload : Var... | def file_transfer_protocol_encode(self, target_network, target_system, target_component, payload):
'''
File transfer message
target_network : Network ID (0 for broadcast) (uint8_t)
target_system : System ID (0 for broadcast) (uint8_... |
File transfer message
target_network : Network ID (0 for broadcast) (uint8_t)
target_system : System ID (0 for broadcast) (uint8_t)
target_component : Component ID (0 for broadcast) (uint8_t)
payload : Var... | def file_transfer_protocol_send(self, target_network, target_system, target_component, payload, force_mavlink1=False):
'''
File transfer message
target_network : Network ID (0 for broadcast) (uint8_t)
target_system : System ID (0 fo... |
Time synchronization message.
tc1 : Time sync timestamp 1 (int64_t)
ts1 : Time sync timestamp 2 (int64_t) | def timesync_send(self, tc1, ts1, force_mavlink1=False):
'''
Time synchronization message.
tc1 : Time sync timestamp 1 (int64_t)
ts1 : Time sync timestamp 2 (int64_t)
'''
return ... |
Camera-IMU triggering and synchronisation message.
time_usec : Timestamp for the image frame in microseconds (uint64_t)
seq : Image frame sequence (uint32_t) | def camera_trigger_send(self, time_usec, seq, force_mavlink1=False):
'''
Camera-IMU triggering and synchronisation message.
time_usec : Timestamp for the image frame in microseconds (uint64_t)
seq : Image frame sequen... |
The global position, as returned by the Global Positioning System
(GPS). This is NOT the global
position estimate of the sytem, but rather a RAW
sensor value. See message GLOBAL_POSITION for the
global position estimate. Coordinate frame i... | def hil_gps_send(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, vn, ve, vd, cog, satellites_visible, force_mavlink1=False):
'''
The global position, as returned by the Global Positioning System
(GPS). This is NOT the global
posit... |
The global position, as returned by the Global Positioning System
(GPS). This is NOT the global
position estimate of the sytem, but rather a RAW
sensor value. See message GLOBAL_POSITION for the
global position estimate. Coordinate frame i... | def hil_gps_encode(self, time_usec, fix_type, lat, lon, alt, eph, epv, vel, vn, ve, vd, cog, satellites_visible):
'''
The global position, as returned by the Global Positioning System
(GPS). This is NOT the global
position estimate of the ... |
Simulated optical flow from a flow sensor (e.g. PX4FLOW or optical
mouse sensor)
time_usec : Timestamp (microseconds, synced to UNIX time or since system boot) (uint64_t)
sensor_id : Sensor ID (uint8_t)
integration_time_us ... | def hil_optical_flow_encode(self, time_usec, sensor_id, integration_time_us, integrated_x, integrated_y, integrated_xgyro, integrated_ygyro, integrated_zgyro, temperature, quality, time_delta_distance_us, distance):
'''
Simulated optical flow from a flow sensor (e.g. PX4FLOW or optical
... |
Sent from simulation to autopilot, avoids in contrast to HIL_STATE
singularities. This packet is useful for high
throughput applications such as hardware in the loop
simulations.
time_usec : Timestamp (microseconds since UNIX epoch or micr... | def hil_state_quaternion_encode(self, time_usec, attitude_quaternion, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, ind_airspeed, true_airspeed, xacc, yacc, zacc):
'''
Sent from simulation to autopilot, avoids in contrast to HIL_STATE
singularities. This pac... |
Sent from simulation to autopilot, avoids in contrast to HIL_STATE
singularities. This packet is useful for high
throughput applications such as hardware in the loop
simulations.
time_usec : Timestamp (microseconds since UNIX epoch or micr... | def hil_state_quaternion_send(self, time_usec, attitude_quaternion, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, ind_airspeed, true_airspeed, xacc, yacc, zacc, force_mavlink1=False):
'''
Sent from simulation to autopilot, avoids in contrast to HIL_STATE
sin... |
The RAW IMU readings for secondary 9DOF sensor setup. This message
should contain the scaled values to the described
units
time_boot_ms : Timestamp (milliseconds since system boot) (uint32_t)
xacc : X acceleration (mg) (i... | def scaled_imu2_encode(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
'''
The RAW IMU readings for secondary 9DOF sensor setup. This message
should contain the scaled values to the described
units
time_boot_m... |
The RAW IMU readings for secondary 9DOF sensor setup. This message
should contain the scaled values to the described
units
time_boot_ms : Timestamp (milliseconds since system boot) (uint32_t)
xacc : X acceleration (mg) (i... | def scaled_imu2_send(self, time_boot_ms, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag, force_mavlink1=False):
'''
The RAW IMU readings for secondary 9DOF sensor setup. This message
should contain the scaled values to the described
units
... |
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