The　aim　of　the　traditional　aerodynamic　control　is　to　change　the　aerial　vehicle　attack　angle　by　angular　motion　induced　by　a　moment,　which　is　generated　by　deflecting　its　control　surfaces,　so　as　to　make　it　be　able　to　generate　pneumatic　lift　and　obtain　the　expected　lateral　acceleration.　However,　this　maneuvering　process　will　result　in　a　delay　between　sending　and　conducting　of　command　signals.　Compared　with　the　aerodynamic　control　mode,　in　the　direct　lateral　thrust　control　mode,　the　lateral　control　jet　engine　is　used　to　generate　control　force　and　torque.　Therefore,　in　this　paper　a　combined　control　mode　of　lateral　thrust　and　aerodynamic　force　is　proposed　to　solve　the　problem　of　rapid　response　and　high　available　overload.　First,　the　control　scheme　is　established　using　the　aerodynamic　control　as　the　main　input　and　the　reaction-jet　control　system　(RCS)　as　the　auxiliary　input.　Then　the　dynamic　and　kinematics　mathematic　model　of　the　aerial　vehicle　is　built　based　on　the　direct　lateral　thrust　control.　As　the　final　step,　aiming　at　the　task　of　terminal　stage　of　the　aerial　vehicle　to　attack　the　target　from　the　top,　the　combined　control　system　is　designed　according　to　fuzzy　adaptive　algorithm.　Simulation　results　indicate　that　the　overload　required　under　the　combined　control　is　lower　than　that　under　the　aerodynamic　control.　So　this　combined　control　system　can　satisfy　the　requirements　of　the　aerial　vehicle　overload　better　than　the　traditional　mode　does.