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在已设计出的飞机总能量控制系统核心环节的基础上，研究了各种高度和速度控制模态下系统的构成和工作原理；研究了各种非线性安全保护功能在系统中的设置与实现；分析了极限推力状态下，飞机质点能量运动的特点；研究了对轨迹和速度的控制优先级的设置与实现技术；最后对此非线性多变量控制系统进行了综合与仿真，得到了满意的设计与仿真结果。
Based on the design of the core of aircraft total energy control system, the composition and working principle of the system under various modes of altitude and speed control were studied. The setting and implementation of various non-linear safety protection functions in the system The characteristics of the energy movement of aircraft mass under the condition of ultimate thrust are analyzed. The setting and realization of control priority of trajectory and velocity are studied. Finally, the nonlinear multivariable control system is integrated and simulated, and the satisfactory Design and simulation results.