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 * modification, are permitted provided that the following conditions
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/**
 * @file tiltrotor_params.c
 * Parameters for vtol attitude controller.
 *
 * @author Roman Bapst <roman@px4.io>
 */

/**
 * Position of tilt servo in mc mode
 *
 * @min 0.0
 * @max 1.0
 * @increment 0.01
 * @decimal 3
 * @group VTOL Attitude Control
 */
PARAM_DEFINE_FLOAT(VT_TILT_MC, 0.0f);

/**
 * Position of tilt servo in transition mode
 *
 * @min 0.0
 * @max 1.0
 * @increment 0.01
 * @decimal 3
 * @group VTOL Attitude Control
 */
PARAM_DEFINE_FLOAT(VT_TILT_TRANS, 0.3f);

/**
 * Position of tilt servo in fw mode
 *
 * @min 0.0
 * @max 1.0
 * @increment 0.01
 * @decimal 3
 * @group VTOL Attitude Control
 */
PARAM_DEFINE_FLOAT(VT_TILT_FW, 1.0f);

/**
 * Tilt actuator control value commanded when disarmed and during the first second after arming.
 *
 * This specific tilt during spin-up is necessary for some systems whose motors otherwise don't
 * spin-up freely.
 *
 * @min 0.0
 * @max 1.0
 * @increment 0.01
 * @decimal 3
 * @group VTOL Attitude Control
 */
PARAM_DEFINE_FLOAT(VT_TILT_SPINUP, 0.0f);

/**
 * Duration of front transition phase 2
 *
 * Time in seconds it should take for the rotors to rotate forward completely from the point
 * when the plane has picked up enough airspeed and is ready to go into fixed wind mode.
 *
 * @unit s
 * @min 0.1
 * @max 5.0
 * @increment 0.01
 * @decimal 3
 * @group VTOL Attitude Control
 */
PARAM_DEFINE_FLOAT(VT_TRANS_P2_DUR, 0.5f);