At present, vertical launch missile with high aspect ratio, but due to the aerodynamic coupling of the large angle of attack during the turning section, the inevitable torsion error of the wing structure, the deflection of the engine thrust and the influence of the gas vane flake, the inclined channel of the missile has a wide rangecomplex interference moment. This paper analyzes the interference moment of the inclined channel, and proposes a control method which is easy to implement in engineering against a wide range complex interference moment. The control scheme combines adaptive limiting and model reference control can effectively suppress the complex interference moment of the inclined channel. After verification by simulation experiment and flight test, the tilt and stability control of the vertical launch missile are achieved and meets the design requirements of the weapon system.