print into the buffer, expanding if needed */

Pretty printer.

Sets guided's angular target submode: Using a rotation quaternion, angular velocity, and climbrate or thrust (depends on user option) attitude_quat: I

set a message rate in Hz; 0 for original, -1 to disable

get value

simple 16 bit random number generator */

Reset state

set lateral input as a value from -100 to +100

sqrt_controller calculates the correction based on a proportional controller with piecewise sqrt sections to constrain second derivative.

lazy helper that allocates a storage buffer and does strcpy for us

possibly send a new GPS packet */

update_all - set target and measured inputs to PID controller and calculate outputs target and error are filtered the derivative is then calculated an

update_xy_controller - runs the horizontal position controller correcting position, velocity and acceleration errors. Position and velocity errors are

TODO: sanity checks?

find defaults in firmware

get_speed_z - returns target descent speed in cm/s during missions. Note: always positive

return relative position from home in meters */

return number of active GPS sensors. Note that if the first GPS is not present but the 2nd is then we return 2. Note that a blended GPS solution is tr

send vehicle state to ride along controlers

return number of bits available

replacement for strdup */

return a wind estimation vector, in m/s; returns 0,0,0 on failure

clear mision_type from autopilot. Note that this does NOT actually send a MISSION_CLEAR_ALL message

arming.disarm - disarm motors

Show errors.

return first bit set, or -1 if none set

return the current airspeed in m/s

get the time-allowed-per-loop in seconds

get MIN/MAX/TRIM parameters

get_rate - returns target rate in deg/sec held in RATE parameter

* get_velocity_z_up_cms - returns the current z-axis velocity, frame z-axis up, in cm/s * * @return z-axis velocity, frame z-axis up, in cm/s */

initialise QAUTOTUNE mode */

move location in metres

num_commands - returns total number of commands in the mission this number includes offset 0, the home location

crc8 from trone driver by Luis Rodrigues */

! * Decode a float from a byte stream by inverse floating point scaling from 1 * unsigned byte. * \param bytes is a pointer to the byte stream to d

! * Encode a float on a byte stream by floating point scaling to fit in 1 * unsigned byte. * \param value is the number to encode. * \param bytes

Return 321-intrinsic euler angles in centidegrees representing the rotation from NED earth frame to the attitude controller's target attitude. NOTE**

return 24 bit bus identifier

** Format and emit an 'iABC' instruction. (Assertions check consistency ** of parameters versus opcode.) */

number of locked satellites

set_pos_target_z_from_climb_rate_cm - adjusts target up or down using a commanded climb rate in cm/s using the default position control kinematic path

Wait for distance to home to be within specified bounds.

Wait for flight of a given distance.

Enable or disable body-frame feed forward

Get Saved parameters.

true if the mode sets the vehicle destination, which controls whether control input is ignored with STICK_MIXING=0

return verbose dump of m. Wraps the pymavlink routine which inconveniently takes a filehandle

get motor interlock status. true means motors run, false motors don't run