Controlled Parameter Selection in Solid Ducted Ramjet for Thrust Control

The selection of controlled parameters of ramjet engine is the foundation of the ramjet engine control system design . The basic principle s for the selection of controlled parameters of the c ontrol system are analyzed in this paper , and the thrust control of ramjet is also analyzed , and it is found un feasible to select the thrust variable as the controlled parameter directly . Then, the selection of intermediate variable as controlled parameter for thrust control is proposed. The ideal thermal cycle of solid ducted ramjet is analyzed, and a steady model of solid ducted ramjet is estimated. T he performance of solid ducted rocket is simulated, the result s show that t here is a one to one correspond ence between the value of � � + = � =