An apparatus for cyclic control for a rotorcraft, the apparatus comprising: a cyclic stick; a mounting frame; a pitch actuator; a pitch force sensor; a roll actuator; a roll force sensor; a stick base assembly coupled with the cyclic stick and configured to rotate with respect to the mounting frame to control a pitch and a roll of the rotorcraft, wherein the stick base assembly includes a tubular body and a stick receiving member protruding therefrom which is configured to receive a base end of the cyclic stick; and a cyclic housing pivotably coupled with the mounting frame for rotation of the cyclic housing and the stick base assembly together about a pitch axis to control the pitch of the rotorcraft, and coupled with the pitch actuator to assist the rotation about the pitch axis, wherein the pitch force sensor coupled between the pitch actuator and the mounting frame measures a resistance applied to the rotation by the pitch actuator, the cyclic housing configured to support the stick base assembly for independent rotation of the stick base assembly about a roll axis to control the roll of the rotorcraft, wherein the stick base assembly couples with the roll actuator to assist the independent rotation about the roll axis, and the roll force sensor coupled between the roll actuator and the cyclic housing measures a resistance applied to the independent rotation by the roll actuator, wherein the cyclic housing includes a structural frame including: a bottom portion rotatably mounted to the mounting frame and including a first hollow passage along the pitch axis for receiving the pitch actuator that rotates about the pitch axis to control the pitch of the rotorcraft; and a top portion disposed above the bottom portion and including a second hollow passage along the roll axis for receiving the roll actuator that rotates about the roll axis to control the roll of the rotorcraft, wherein the roll axis is perpendicular to the pitch axis. a cyclic stick; a mounting frame; a pitch actuator; a pitch force sensor; a roll actuator; a roll force sensor; a stick base assembly coupled with the cyclic stick and configured to rotate with respect to the mounting frame to control a pitch and a roll of the rotorcraft, wherein the stick base assembly includes a tubular body and a stick receiving member protruding therefrom which is configured to receive a base end of the cyclic stick; and a cyclic housing pivotably coupled with the mounting frame for rotation of the cyclic housing and the stick base assembly together about a pitch axis to control the pitch of the rotorcraft, and coupled with the pitch actuator to assist the rotation about the pitch axis, wherein the pitch force sensor coupled between the pitch actuator and the mounting frame measures a resistance applied to the rotation by the pitch actuator, the cyclic housing configured to support the stick base assembly for independent rotation of the stick base assembly about a roll axis to control the roll of the rotorcraft, wherein the stick base assembly couples with the roll actuator to assist the independent rotation about the roll axis, and the roll force sensor coupled between the roll actuator and the cyclic housing measures a resistance applied to the independent rotation by the roll actuator, wherein the cyclic housing includes a structural frame including: a bottom portion rotatably mounted to the mounting frame and including a first hollow passage along the pitch axis for receiving the pitch actuator that rotates about the pitch axis to control the pitch of the rotorcraft; and a top portion disposed above the bottom portion and including a second hollow passage along the roll axis for receiving the roll actuator that rotates about the roll axis to control the roll of the rotorcraft, wherein the roll axis is perpendicular to the pitch axis.