In this paper, it was mainly studied that how to realize the modularity general-purpose and miniaturization of launch control system which was based on common-frame launch.

This thesis combines with the pre-research requirements of a certain common-frame launch system, by means of multi-rigid-body dynamic theories and visual prototype technology, the research has been done on the initial designing of the common-frame launch system, launching characteristic simulation, the dynamic s.

The thermal safety of common vertical launch compartment is the most important factor of the safety of launch system, research of launch compartment fire can forecast the missile thermal environment, it can provide theoretical support for the safety research and design of launch compartment.

It has discussed the electronic control skills for the common frame of launching equipment about carrier missiles, expatiated the composing of standard and common control system for carrier missile common frame of launching equipments, it stressed the designing idea for common and reliability.

This paper introduces the application of hybrid programming in the AAM launcher automatic test and measurement system.

This paper briefly introduces the method constitued the interface of air-to-air missile launcher automatic test and measurement system by applying multichannel ADC, DAC and depicts its working principle in the system.