The invention relates to a fault-adaptive carrier rocket intelligent control semi-physical simulation method, and belongs to the technical field of carrier rocket semi-physical simulation. The methodcomprises the steps: step 1, establishing a carrier rocket six-degree-of-freedom simulation model including a kinetic model, a mass model, a gravitational attraction model, an aerodynamic force model,an engine model and a sensor model; step 2, establishing a GNC model of the carrier rocket comprising a navigation model, a guidance model and a control model; step 3, establishing a real-time faultdetection and isolation model; judging whether the engine has a fault or not according to the real-time fault detection and isolation model; step 4, planning an optimal trajectory curve of the rocketafter any fault. According to the invention, the adaptability to rocket faults is realized, a semi-physical simulation system based on a carrier rocket six-degree-of-freedom simulation computer and highly integrated rocket-borne comprehensive electronics is built, so that the semi-physical simulation verification of rocket intelligent control in a fault state is realized.