Aircraft Thrust Scheme Optimization Hybrid Program Based on Simulink-M

Hybrid programming based on Simulink-M file, that can improve the program execution effectively, is proposed. The problems that it is hard to cycle and search in high efficiency in Simulink and that it is hard to build and modify the program model in M file are solved. By this method, simulation program for the optimization of specific aircraft thrust scheme is worked out. Global optimization for potential schemes in the three different thrusts is accomplished, and the optimized results for different thrusts obtained by comparison. It is indicated that the method has good practicality.