In recent years, most of high performance aircrafts have been designing by the Active Control Technology (ACT) in order to realize the CAS, RSS, MLC, DFC, FMC and so on.
This paper deals with the problem of constucting the two advanced flight control systems such as DFC and vertical CAS. Decoupling control theory, model matching theory and model following servo controller approaches applied in order to solve these problems.
First, by using the decoupling theory, flight control laws have been determined for the six open loop CCV modes. Next, the C model following flight control systems which design the vertical CAS are constructed both by using the model matching theory and the model following servo controller scheme. Simulation studies for designing the advanced flight controller of supersonic aircraft are presented in order to demonstrate the effectiveness of the proposed approaches.
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