uuv_att_control_params.c 3.67 KB
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/**
 * @file uuv_att_control_params.c
 *
 * Parameters defined by the attitude control task for unmanned underwater vehicles (UUVs)
 *
 * This is a modification of the fixed wing/ground rover params and it is designed for ground rovers.
 * It has been developed starting from the fw  module, simplified and improved with dedicated items.
 *
 * All the ackowledgments and credits for the fw wing/rover app are reported in those files.
 *
 * @author Daniel Duecker <daniel.duecker@tuhh.de>
 */

/*
 * Controller parameters, accessible via MAVLink
 *
 */

// Roll gains
/**
 * Roll proportional gain
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_ROLL_P, 4.0f);

/**
 * Roll differential gain
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_ROLL_D, 1.5f);


// Pitch gains
/**
 * Pitch proportional gain
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_PITCH_P, 4.0f);

/**
 * Pitch differential gain
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_PITCH_D, 2.0f);


// Yaw gains
/**
 * Yawh proportional gain
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_YAW_P, 4.0f);

/**
 * Yaw differential gain
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_YAW_D, 2.0f);


// Input Modes
/**
 * Select Input Mode
 *
 * @value 0 use Attitude Setpoints
 * @value 1 Direct Feedthrough
 * @group UUV Attitude Control
 */
PARAM_DEFINE_INT32(UUV_INPUT_MODE, 0);

/**
 * Skip the controller
 *
 * @value 0 use the module's controller
 * @value 1 skip the controller and feedthrough the setpoints
 */
PARAM_DEFINE_INT32(UUV_SKIP_CTRL, 0);

/**
 * Direct roll input
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_DIRCT_ROLL, 0.0f);

/**
 * Direct pitch input
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_DIRCT_PITCH, 0.0f);

/**
 * Direct yaw input
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_DIRCT_YAW, 0.0f);

/**
 * Direct thrust input
 *
 * @group UUV Attitude Control
 */
PARAM_DEFINE_FLOAT(UUV_DIRCT_THRUST, 0.0f);