提出了现代飞行控制系统的优化设计需考虑驾驶员的操纵行为和生理限制，才能进行人-机组合优化设计。
This paper proposes that it is necessary to concern the pilot's control behavior and human limits during the optimal design of modern flight controlling system.
现代飞机飞行控制系统的设计需求和特征，对传统的现代控制设计方法提出了挑战。
Design requirements and features for modern flight control systems presents a challenge to traditional design methods for flight control systems.
为了获得更好的飞行品质，许多现代控制方法被应用到飞机飞行控制系统中。
To obtain the better flight qualities, many modern control methods are applied in the design of aircraft flight control systems.
现代无人直升机飞行控制系统一般由飞行控制计算机、伺服驱动机构、传感器、地面监测控制等分系统组成。
The modern unmanned helicopter flight control system is generally composed of the flight control computer, the servo driving mechanism, the sensor, and the ground monitor control system etc.
通过分析控制律结构、设计方法以及系统调参方法，建立了能够反映现代战斗机飞行控制系统主要功能的控制律设计方法。
By analyzing the structures, designing methods and gain scheduling methods of FCL, the designing techniques of FCL which can indicate the main functions of modern fighters' FCS are established.
例如在现代飞行器中，动力助推控制系统将飞行员的力放大以推动受到很大的气流作用的机翼表面。
In a modern aircraft, for example, the power boost controls amplify the force applied by the pilot to move the control surface against large aerodynamic forces.
例如在现代飞行器中，动力助推控制系统将飞行员的力放大以推动受到很大的气流作用的机翼表面。
In a modern aircraft, for example, the power boost controls amplify the force applied by the pilot to move the control surface against large aerodynamic forces.
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