Abstract
According to the stability requirement of the missile launcher in operating the portable missile launching control device, a structure is designed. Firstly, the structural mechanics theory method is used to analyse the deflection of the outrigger. The force bending of the sector plate is analysed and the bending displacement of the rigid frame after the column is simplified is analysed. Then the main structure of the portable missile launching device is given and the stability of the outrigger, base and column system is analysed and simulated by ANSYS and ADAMS simulation software respectively. Finally, the stability of the equipment was tested to verify the calculation and analysis of the stability of the device. The feasibility and rationality of the design of the portable missile launching device was confirmed.
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