When the aircraft vibration balancer is working in 3D mode, if the aircraft is performing acrobatic flight, the balancer will sense the roll rate and flight attitude of the three axial directions through the gyroscope, and give the automatic control quantity through corresponding control of the rudder surface, so that the aircraft tends to maintain the current attitude. The balancing instrument has no requirements on the operating environment, and can be used in various weather conditions or indoors. After installation, no other initialization process is required, and the aircraft can take off after power is turned on.

In order to reduce the burden of users after flight, a balance instrument module can be added to the aircraft and inserted between RC receiver and steering engine. In other words, PMW signals sent by RC transmitter can reach the steering engine only after being transferred by the balance instrument, instead of being in a direct state. Two modes are thus generated: manual mode and stabilization mode. In manual mode, the balance instrument transfers signals from RC transmitter almost intact, and of course, necessary mixed control processing must be carried out for the flying wing type (aileron lifting mixed control) and v-tail type (lifting direction mixed control).

Airline vibration balancing instrument integrated three-axis gyroscope, three-axis accelerometer, basic inertial navigation platform of the plane is obtained by calculating inertial strapdown attitude algorithm of flight attitude. When working in automatic balance model of the vibration balancing instrument, once to detect the aircraft's attitude and the Angle between the horizontal line to produce change, it will signal correction control aircraft flap rudder, elevator and rudder to keep the balance of the aircraft. Constant modification by the aero vibration balancer will automatically return the aircraft to a balanced flight posture. The cyclic controls the aircraft's pitch (up or down), the ailerons control the aircraft's roll, and the rudder corrects the aircraft's direction to the left or right. Aircraft controllers simply place the lever in the middle and the aircraft automatically returns to a balanced flying position.