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A mixed linear parameter-varying (LPV)/mu technique is applied to global control of an air defense missile. The technique is a direct extension of mu-synthesis that additionally incorporates the gain-scheduling task and makes the time-varying nature of the plant be explicitly taken into account. By use of the technique, an LPV controller is designed based on a model matching control structure. The...
The dynamic characteristics of missile vary substantially with flight conditions such as flight Mach number, altitude and angle of attack. Therefore, in order to achieve adequate levels of robustness and performance, a controller that also varies during operation has to be designed in missile control. This paper is concerned with the application of advanced mixed linear parameter-varying (LPV)/mu...
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