Write tiltrotor specific log

constructor for a response structure

---------------------------------------------------------------------------- switch to Idle mode

assert channel value is within the range [value_min, value_max]

bind the socket */

updates a Blake2 hash with a 32 bit word, little endian.

calibrate the barometer. This must be called at least once before the altitude() or climb_rate() interfaces can be used

returns true if the destination is within fence (used to reject waypoints outside the fence)

consumed_mah - returns total current drawn since start-up in milliampere.hours

disable interrupts and return a context that can be used to restore the interrupt state. This can be used to protect critical regions */

this is _expect_delay_ms() with check that we are in the main thread */

force safety on

get current position source

Return body-frame feed forward setting

return body-frame yaw angle from a mount target

return address on bus

return low pass filtered loop rate in hz

get forward speed in m/s (earth-frame horizontal velocity but only along vehicle x-axis). returns true on success

get_max_speed_xy_cms - get the maximum horizontal speed in cm/s

get a twos-complement value from the first 'length' bits of a uint32_t With thanks to betaflight */

map a user pin number to a GPIO table entry */

returns true if we've ever seen RC input, via overrides or via AP_RCProtocol

Check basic filter health metrics and return a consolidated health status

Takeoff and hover, checking the noise against the provided db level and returning peak db

setup the identity matrix

input_pos_vel_accel_z - calculate a jerk limited path from the current position, velocity and acceleration to an input position velocity and accelerat

Command a thrust vector and heading rate

return whether the group channel is both enabled in the group and for output

timestamp of most recent data read from the sensor

Return configured tilt angle limit in centidegrees

lock the DMA channels, blocking method

get longitude scale factor

** Ensures the stack has at least 'space' extra slots, raising an error ** if it cannot fulfill the request. (The error handling needs a few ** extra

** Create or reuse a zero-terminated string, first checking in the ** cache (using the string address as a key). The cache can contain ** only zero-te

de-activate the relay

on - turns the buzzer on or off

read len bytes without advancing the read pointer */

* fly_forward is set by the vehicles to indicate the vehicle * should generally be moving in the direction of its heading. * It is an additi

set_pos_desired_z_cm - set altitude target in cm above the EKF origin

check how much stack is free given a stack base. Assumes the fill byte is 0x55 */

* Documented in the header file. */

return 64 bit x / 1000 faster than the normal gcc implementation using by about 3x With thanks to https://0x414b.com/2021/04/16/arm-division.html

Updates the parameter documentation in the target file or in all *.param,*.parm files of the target directory. This function iterates over a

return true if the current AHRS airspeed estimate is directly derived from an airspeed sensor */

Wait for local target velocity

return true if this is a watchdog reset boot and we were armed

Initialise the filter

return estimate of true airspeed vector in body frame in m/s returns false if estimate is unavailable

check settings are valid

Attach an interrupt handler to a GPIO pin number. The pin number must be one specified with a GPIO() marker in hwdef.dat */

calculate a new nav_roll_cd from the navigation controller */

Copy the variable's whole name to the supplied buffer. If the variable is a group member, prepend the group name.

crc8 from betaflight

free memory from a heap */

terrain failsafe action

force safety off

Generate a launch description for SITL.

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

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