CTS test method for cartridge clip type machine-ammunition separation

The invention relates to a CTS test method for cartridge clip type aircraft-missile separation, and aims to establish a simulation test method for a whole process of backward separation and release of an embedded missile from a high-density cartridge clip type missile cabin of a novel aircraft in a wind tunnel. The method comprises a trajectory capturing method for guided missile limited linear motion (sliding rail sections of two sliding blocks), guided missile rotation motion (single sliding block) and guided missile unconstrained free motion (no sliding block), a wind tunnel test is carried out by adopting the trajectory capturing method, and the trajectory and attitude angle change in the backward separation process of the embedded missile and the cartridge clip type aircraft are obtained. Determining the safety of separation; the method has the advantage of high authenticity of simulating a cartridge clip type machine-missile separation scene, and deduces dynamics and kinematics equations of limited line