Spelling errors (#19935)

This commit is contained in:
Hamish Willee
2022-07-27 14:33:16 +10:00
committed by GitHub
parent 97f632a408
commit e6eed43648
97 changed files with 170 additions and 158 deletions
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@@ -5,6 +5,6 @@ float32 indicated_airspeed_m_s # indicated airspeed in m/s
float32 true_airspeed_m_s # true filtered airspeed in m/s
float32 air_temperature_celsius # air temperature in degrees celsius, -1000 if unknown
float32 air_temperature_celsius # air temperature in degrees Celsius, -1000 if unknown
float32 confidence # confidence value from 0 to 1 for this sensor
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@@ -21,7 +21,7 @@ uint16 capacity # actual capacity of the battery
uint16 cycle_count # number of discharge cycles the battery has experienced
uint16 average_time_to_empty # predicted remaining battery capacity based on the average rate of discharge in min
uint16 serial_number # serial number of the battery pack
uint16 manufacture_date # manufacture date, part of serial number of the battery pack. formated as: Day + Month×32 + (Year1980)×512
uint16 manufacture_date # manufacture date, part of serial number of the battery pack. Formatted as: Day + Month×32 + (Year1980)×512
uint16 state_of_health # state of health. FullChargeCapacity/DesignCapacity, 0-100%.
uint16 max_error # max error, expected margin of error in % in the state-of-charge calculation with a range of 1 to 100%
uint8 id # ID number of a battery. Should be unique and consistent for the lifetime of a vehicle. 1-indexed.
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@@ -17,7 +17,7 @@ uint8 CELLULAR_STATUS_FLAG_CONNECTED=12 # One or more packet data bearers is ac
uint8 CELLULAR_NETWORK_FAILED_REASON_NONE=0 # No error
uint8 CELLULAR_NETWORK_FAILED_REASON_UNKNOWN=1 # Error state is unknown
uint8 CELLULAR_NETWORK_FAILED_REASON_SIM_MISSING=2 # SIM is required for the modem but missing
uint8 CELLULAR_NETWORK_FAILED_REASON_SIM_ERROR=3 # SIM is available, but not usuable for connection
uint8 CELLULAR_NETWORK_FAILED_REASON_SIM_ERROR=3 # SIM is available, but not usable for connection
uint16 status # Status bitmap 1: Roaming is active
uint8 failure_reason #Failure reason when status in in CELLUAR_STATUS_FAILED
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@@ -5,6 +5,6 @@ uint32 device_id # unique device ID for the sensor that does
float32 differential_pressure_pa # differential pressure reading in Pascals (may be negative)
float32 temperature # Temperature provided by sensor in celcius, NAN if unknown
float32 temperature # Temperature provided by sensor in degrees Celsius, NAN if unknown
uint32 error_count # Number of errors detected by driver
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@@ -30,7 +30,7 @@ bool gps_data_stopped_using_alternate # 3 - true when the gps data has stoppe
bool height_sensor_timeout # 4 - true when the height sensor has not been used to correct the state estimates for a significant time period
bool stopping_navigation # 5 - true when the filter has insufficient data to estimate velocity and position and is falling back to an attitude, height and height rate mode of operation
bool invalid_accel_bias_cov_reset # 6 - true when the filter has detected bad acceerometer bias state esitmstes and has reset the corresponding covariance matrix elements
bool bad_yaw_using_gps_course # 7 - true when the fiter has detected an invalid yaw esitmate and has reset the yaw angle to the GPS ground course
bool bad_yaw_using_gps_course # 7 - true when the filter has detected an invalid yaw estimate and has reset the yaw angle to the GPS ground course
bool stopping_mag_use # 8 - true when the filter has detected bad magnetometer data and is stopping further use of the magnetomer data
bool vision_data_stopped # 9 - true when the vision system data has stopped for a significant time period
bool emergency_yaw_reset_mag_stopped # 10 - true when the filter has detected bad magnetometer data, has reset the yaw to anothter source of data and has stopped further use of the magnetomer data
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@@ -18,8 +18,8 @@ float32 rng_vpos # range sensor height innovation (m) and innovation variance (m
float32 baro_vpos # barometer height innovation (m) and innovation variance (m**2)
# Auxiliary velocity
float32[2] aux_hvel # horizontal auxiliar velocity innovation from landing target measurement (m/sec) and innovation variance ((m/sec)**2)
float32 aux_vvel # vertical auxiliar velocity innovation from landing target measurement (m/sec) and innovation variance ((m/sec)**2)
float32[2] aux_hvel # horizontal auxiliary velocity innovation from landing target measurement (m/sec) and innovation variance ((m/sec)**2)
float32 aux_vvel # vertical auxiliary velocity innovation from landing target measurement (m/sec) and innovation variance ((m/sec)**2)
# Optical flow
float32[2] flow # flow innvoation (rad/sec) and innovation variance ((rad/sec)**2)
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@@ -9,7 +9,7 @@ bool cs_yaw_align # 1 - true if the filter yaw alignment is complet
bool cs_gps # 2 - true if GPS measurement fusion is intended
bool cs_opt_flow # 3 - true if optical flow measurements fusion is intended
bool cs_mag_hdg # 4 - true if a simple magnetic yaw heading fusion is intended
bool cs_mag_3d # 5 - true if 3-axis magnetometer measurement fusion is inteded
bool cs_mag_3d # 5 - true if 3-axis magnetometer measurement fusion is intended
bool cs_mag_dec # 6 - true if synthetic magnetic declination measurements fusion is intended
bool cs_in_air # 7 - true when the vehicle is airborne
bool cs_wind # 8 - true when wind velocity is being estimated
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@@ -3,7 +3,7 @@
uint64 timestamp # time since system start (microseconds)
uint8 instance # Instance of GNSS reciever
uint8 instance # Instance of GNSS receiver
uint8 len # length of data, MSB bit set = message to the gps device,
# clear = message from the device
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@@ -29,8 +29,8 @@ int32 rssi # receive signal strength indicator (RSSI): < 0: Undefined, 0: no
bool rc_failsafe # explicit failsafe flag: true on TX failure or TX out of range , false otherwise. Only the true state is reliable, as there are some (PPM) receivers on the market going into failsafe without telling us explicitly.
bool rc_lost # RC receiver connection status: True,if no frame has arrived in the expected time, false otherwise. True usually means that the receiver has been disconnected, but can also indicate a radio link loss on "stupid" systems. Will remain false, if a RX with failsafe option continues to transmit frames after a link loss.
uint16 rc_lost_frame_count # Number of lost RC frames. Note: intended purpose: observe the radio link quality if RSSI is not available. This value must not be used to trigger any failsafe-alike funtionality.
uint16 rc_total_frame_count # Number of total RC frames. Note: intended purpose: observe the radio link quality if RSSI is not available. This value must not be used to trigger any failsafe-alike funtionality.
uint16 rc_lost_frame_count # Number of lost RC frames. Note: intended purpose: observe the radio link quality if RSSI is not available. This value must not be used to trigger any failsafe-alike functionality.
uint16 rc_total_frame_count # Number of total RC frames. Note: intended purpose: observe the radio link quality if RSSI is not available. This value must not be used to trigger any failsafe-alike functionality.
uint16 rc_ppm_frame_length # Length of a single PPM frame. Zero for non-PPM systems
uint8 input_source # Input source
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@@ -4,7 +4,7 @@ uint16 tx_buf_write_index # current size of the tx buffer
uint16 rx_buf_read_index # the rx buffer is parsed up to that index
uint16 rx_buf_end_index # current size of the rx buffer
uint16 failed_sbd_sessions # number of failed sbd sessions
uint16 successful_sbd_sessions # number of successfull sbd sessions
uint16 successful_sbd_sessions # number of successful sbd sessions
uint16 num_tx_buf_reset # number of times the tx buffer was reset
uint8 signal_quality # current signal quality, 0 is no signal, 5 the best
uint8 state # current state of the driver, see the satcom_state of IridiumSBD.h for the definition
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@@ -24,7 +24,7 @@ uint8 MODE_BLINK_FAST = 5
uint8 MODE_BREATHE = 6 # continuously increase & decrease brightness (solid color if driver does not support it)
uint8 MODE_FLASH = 7 # two fast blinks (on/off) with timing as in MODE_BLINK_FAST and then off for a while
uint8 MAX_PRIORITY = 2 # maxium priority (minimum is 0)
uint8 MAX_PRIORITY = 2 # maximum priority (minimum is 0)
uint8 led_mask # bitmask which LED(s) to control, set to 0xff for all
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@@ -1,4 +1,4 @@
uint64 timestamp # time since system start (microseconds)
float32 indicated_frequency_rpm # indicated rotor Frequency in Revolution per minute
float32 estimated_accurancy_rpm # estimated accurancy in Revolution per minute
float32 estimated_accurancy_rpm # estimated accuracy in Revolution per minute
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@@ -3,6 +3,6 @@ uint64 timestamp_sample
uint32 device_id # unique device ID for the sensor that does not change between power cycles
float32 temperature # Temperature provided by sensor (Celcius)
float32 temperature # Temperature provided by sensor (Celsius)
float32 humidity # Humidity provided by sensor
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@@ -1,4 +1,4 @@
# Status of the takeoff state machine currently just availble for multicopters
# Status of the takeoff state machine currently just available for multicopters
uint64 timestamp # time since system start (microseconds)
@@ -11,4 +11,4 @@ uint8 TAKEOFF_STATE_FLIGHT = 5
uint8 takeoff_state
float32 tilt_limit # limited tilt feasability during takeoff, contains maximum tilt otherwise
float32 tilt_limit # limited tilt feasibility during takeoff, contains maximum tilt otherwise
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@@ -413,7 +413,7 @@ def convert_dir(format_idx, inputdir, outputdir, package, templatedir):
def copy_changed(inputdir, outputdir, prefix='', quiet=False):
"""
Copies files from inputdir to outputdir if they don't exist in
ouputdir or if their content changed
outputdir or if their content changed
"""
# Make sure output directory exists:
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@@ -8,8 +8,8 @@ uint32 sessionid # UWB SessionID
uint32 time_offset # Time between Ranging Rounds in ms
uint16 status # status feedback #
uint16[12] anchor_distance # distance in cm to each UWB Anchor (UWB Device wich takes part in Ranging)
uint16[12] anchor_distance # distance in cm to each UWB Anchor (UWB Device which takes part in Ranging)
bool[12] nlos # Visual line of sight yes/no
float32[12] aoafirst # Angle of arrival of first incomming RX msg
float32[12] aoafirst # Angle of arrival of first incoming RX msg
float32[3] position # Position of the Landing point in relation to the Drone (x,y,z in Meters NED)
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@@ -99,7 +99,7 @@ uint16 VEHICLE_CMD_FIXED_MAG_CAL_YAW = 42006 # Magnetometer calibrati
# PX4 vehicle commands (beyond 16 bit mavlink commands)
uint32 VEHICLE_CMD_PX4_INTERNAL_START = 65537 # start of PX4 internal only vehicle commands (> UINT16_MAX)
uint32 VEHICLE_CMD_SET_GPS_GLOBAL_ORIGIN = 100000 # Sets the GPS co-ordinates of the vehicle local origin (0,0,0) position. |Empty|Empty|Empty|Empty|Latitude|Longitude|Altitude|
uint32 VEHICLE_CMD_SET_GPS_GLOBAL_ORIGIN = 100000 # Sets the GPS coordinates of the vehicle local origin (0,0,0) position. |Empty|Empty|Empty|Empty|Latitude|Longitude|Altitude|
uint8 VEHICLE_MOUNT_MODE_RETRACT = 0 # Load and keep safe position (Roll,Pitch,Yaw) from permanent memory and stop stabilization |
uint8 VEHICLE_MOUNT_MODE_NEUTRAL = 1 # Load and keep neutral position (Roll,Pitch,Yaw) from permanent memory. |
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@@ -32,7 +32,7 @@ float32 y # East position
float32 z # Down position
# Orientation quaternion. First value NaN if invalid/unknown
float32[4] q # Quaternion rotation from FRD body frame to refernce frame
float32[4] q # Quaternion rotation from FRD body frame to reference frame
float32[4] q_offset # Quaternion rotation from odometry reference frame to navigation frame
# Row-major representation of 6x6 pose cross-covariance matrix URT.