Wait for a given vertical rate.

Wait for a given pitch in degrees.

Write a helicopter motors packet

log gyro fft messages

log ahrs home and EKF origin

Update Filter States - this should be called whenever new IMU data is available

Write an attitude packet, targets in degrees

Write an SERVO packet

Write a rate packet

accel_to_angle converts a maximum accel in m/s/s to a lean angle in degrees

accept a new connection. Only valid for TCP connections after listen has been used. A new socket is returned */

check if we are flying as a tailsitter */

add a distance to the temp boundary if it is shorter than any other provided distance since the last time the boundary was reset pitch and yaw are in

random methods that AP_NavEKF3 wants to call on AHRS:

alt_min - returns the min altitude above home the vehicle should have before parachute is released 0 = altitude check disabled

* Documented in the header file */

wait for EKF's accel bias to reach a level and maintain it

rotate a 2D vector from earth frame to body frame

initialise a bouncebuffer */

Alternative interface: */

return define name needed for board.h for ChibiOS

calculate correction from temperature calibration from log data using parameters

copied from AP_FETtecOneWire.cpp

returns a value 0-255 for LED brightness:

arming.disarm - disarm motors

do_pilot_takeoff - controls the vertical position controller during the process of taking off take off is complete when the vertical target reaches th

* Attempt to decode a single channel raw channel datum * * The DSM* protocol doesn't provide any explicit framing, * so we detect dsm frame boundar

return beacon enabled

expand to hold at least num_items

This gets called if mission items are in ALT_ABOVE_TERRAIN frame Terrain failure occurs when terrain data is not found, or rangefinder is not enabled

fill an array of float with NaN, used to invalidate memory in SITL

return the Euler roll, pitch and yaw angle in radians for the specified instance

return filter status flags */

return the amount of NE position change in metres due to the last reset returns the time of the last reset or 0 if no reset has ever occurred

Write the last calculated D position relative to the reference point (m). If a calculated solution is not available, use the best available data and r

Write the last calculated NE position relative to the reference point (m). If a calculated solution is not available, use the best available data and

returns the index of the IMU of the primary core return -1 if no primary core selected

get the yaw acceleration limit in centidegrees/s/s or radians/s/s

get maximum lean angle when using loiter

returns armed state for the current frame

get bearing to target in centi-degrees

return a list of build options

get the power in dbm, rounding appropriately

return the sensor delay in milliseconds (see _DELAY_MS parameter)

get latest desired speed recorded during call to get_throttle_out_speed. For reporting purposes only

return distance (in meters) to destination

get horizontal distance to loiter target in cm

return driver type index i

get filter size

return heading 0-359

returns number of points on the path

Return mask of output channels which the RSC is outputting on

get_phase_angle - returns the rotor phase angle

return the index of the primary core or -1 if no primary core selected

get_safe_alt - returns maximum safe altitude (i.e. alt_max - margin)