This　work　aims　to　present　a　general　composite　laminated　plate-shell　coupled　structure　(CL-PSCS)　model　for　analyzing　the　transient　vibration　properties　subjected　to　continuous　moving　concentrated/distributed　excitations　with　high　velocity.　Thereinto,　arbitrary　constraint　conditions　at　the　coupling/boundary　edges　of　the　structural　system　are　achieved　by　introducing　the　artificial　virtual　point　coupling　technology.　By　using　the　simple　first-order　shear　deformation　theory　(S-FSDT),　the　in-plane　rotational　displacement/moment　overflowing　problem　in　the　original　FSDT　is　effectively　avoided.　Next,　the　limitation　of　the　number　of　coupling　substructures　and　coupling　angle　for　the　CL-PSCS　is　overcome　by　precisely　dividing　the　moving　excitation　into　several　stages　to　imitate　the　uninterrupted　loading　mechanism.　Then,　the　dynamic　responses　are　obtained　accurately　by　employing　the　multistage　inhomogeneous　term　superposition　and　Fourier　series　expansion　in　the　method　of　the　reverberation-ray　matrix　(MRRM).　The　novelty　of　this　paper　is　that　the　global-domain　analysis　for　the　CL-PSCS　under　continuous　moving　excitations　is　achieved　for　the　first　time.　The　accuracy　and　applicability　of　the　present　model　and　method　are　verified　through　the　comparative　evaluations　of　the　common　CL-PSCSs　with　‘‘U＇-shape　type　and　‘‘Ω＇-shape　type.　Moreover,　various　parametric　studies　regarding　the　effects　of　structural　and　excitation　parameters　on　the　vibration　reduction　response　are　discussed.　©　2023　Elsevier　Ltd