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In order to test the validity of active noise control technique in the area of low frequency cabin noise reduction of military transporter, an experimental active noise control system is designed and realized in the paper. Method of shaker plus fuselage panel is adopted to simulate the inner induced noise of the cabin caused by propeller. An adaptive active noise control system based on fore-feed structure is designed to build the system, in which the FX-LMS algorithm is introduced in design of the controller. A set of monitoring microphones are used to monitor the effect of noise reduction. The experimental target is well reached according to experimental results. It also shows that space between primary and secondary loudspeakers has an important influence on the effect of noise reduction.