Abstract
Missile attitude control system usually adopts fixed gain with feedback control and the design method of combining with using the classical autopilot approach. But the missile’s dynamic characteristics and parameters varies with the environment changes dramatically, the traditional method is sometimes hard to meet the guidance performance requirements. According to the missile control system as the research object, based on the theory of adaptive control of missile attitude stabilization loop control method, and LabVIEW control simulation development environment to achieve the model reference adaptive control simulation software module, and the design of missile attitude control system simulation experiment. This design method can be used for missile attitude control system analysis, design and effectively assisting the designer to design the control system, simulation, optimization and programming, the linear system and nonlinear system by computer simulation, through adjustment of controller parameters to obtain satisfactory control effect online. It has a certain practical reference value for the actual design work.Keywordsmodel reference adaptive control(MRAC)LabVIEWattitude control system
Published Version
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