So making researches on the light aircraft flight control system is of theory, engineering and economical value.
研究小型飞机的飞行控制系统具有重要的理论意义、工程意义和经济意义。
As the power source of the aircraft flight control system and landing gear loads, aircraft hydraulic system plays a key role for the safety of aircraft flying.
飞机液压系统作为飞机飞行控制系统和起落架等负载的动力源，对飞机的安全飞行起着关键的作用。
A state-of-the-art aircraft flight control system has electronic rather than mechanical controls and operation is combined with computer technology to maintain the vehicle's stability.
此外，它运用目前最先进的电子操控系统，取代机械式系统，并结合了计算机科技来维持其稳定性。
ABL will now undergo flight tests in which the aircraft will fire its high-energy laser, first into an onboard calorimeter, then through its beam control/fire control system.
ABL现在将接受一系列的飞行测试，飞机将发射高能激光，第一次到板载热量计，然后通过其光束控制/火力控制系统。
Monitoring and redundancy within the flight control system, aircraft sensors, power and hydraulic generation ensure a high degree of availability of the electrical control.
飞行操纵系统的监控和冗余、飞机传感器、动力和液压的产生，这些构成了高度有效性的电传操纵。
The paper introduces the flight control system of the pilotless aircraft.
本文介绍“长空”超低空无人驾驶飞机的飞行控制系统。
This paper presents mainly parameter selection characteristic of autopilot and effect to flight quality of aircraft, after a basic configuration of fixed gain control augmentation system is shown.
文中在给出了固定增益的控制增稳系统的基本组成之后，着重介绍自动驾驶仪的参数选择特点及其对飞机飞行品质的影响。
The paper analyses the launching missiles stability of aircraft with auto-flight system, and simulates the process of launching and optimizes the control law of the auto-flight system.
文中对带有自动驾驶仪飞机投弹的稳定性进行了分析，对其过程进行了仿真研究和控制律优化设计。
All the MH-60Gs have an automatic flight control system to stabilize the aircraft in typical flight altitudes.
全部的MH - 60g都装备了自动飞行控制系统，可将飞机保持在特定飞行高度上。
The system adopts full authority DFBW for aircraft, which may change the characteristics of control feel, handling system and longitudinal short-period aerodynamics during flight.
该系统对飞机实施全权限数字电传操纵，可以在飞行中改变飞机的操纵感觉特性、操纵系统特性和纵向短周期气动特性。
Every part of the aircraft-control system has been fully tested. So, sit back and enjoy your flight since nothing can go wrong.
飞机控制系统的每一个零件都进行过充分的试验。所以请安心坐下，享受你的飞行乐趣，因为不会出什么毛病。
Conventional linear flight control systems do not satisfy nonlinear control requirement of aircraft with thrust vector, which is a multiple control redundances and nonlinear MIMO system.
常规线性飞控系统针对推力矢量飞机这样的多控制冗余、非线性MIMO系统，无法实现非线性控制。
Based on existent conditions of flight control system and avionic system for an aircraft. The paper presents three schemes of automatic terrain anti-collision according to the radar operating way.
本文立足于某飞机飞行控制系统和航空电子系统的现有条件，依据雷达天线的工作方式，提出了三种自动地形防撞的原理方案。
Simulation result indicates that the equivalent moment derivatives model can be used in the evaluation of aircraft conceptual design and flight control system design.
验证表明，等效力矩导数模型可用于评估设计方案或指导飞行控制系统设计。
Taking the lateral flight control system of an aircraft as an example, simulation was carried out for the cases with perturbing parameter and interference.
以某型飞机侧向飞行控制系统为例，针对系统参数摄动和承受有界干扰情况，对所提出的方法进行了仿真分析与验证。
Through ground test, suitable parameters of the structural filter are selected and the coupling between the flight control system and the aircraft elasticity structure is effectively restrained.
通过试验，选择了合适的结构滤波器参数，有效地抑制了飞行控制系统与飞机弹性结构之间的耦合。
In this paper, the authors try to apply neutral stability mode of the aircraft direct force Control technology to the air-to-air gunnery mode of the integrated flight/fire control system.
本文提出飞机中性稳定技术应用于综合火力 /飞行控制系统 ，给出了中性稳定飞机结构图和动力学模型。
Aircraft control system is a key system to ensure flight safety.
飞机操纵系统是一个控制飞机飞行安全的关键系统。
In this paper, the concept of emergency flight control system which USES the engine throttle to manipulate the aircraft in case of control surface failure is discussed.
研究了当飞机常规操纵舵面失效时，通过调节飞机发动机推力大小来操纵飞机的飞行问题。
The atmosphere data measure system plays a very important role in an aircraft system and it provides the height and velocity information and so forth for the flight control system.
大气数据测量系统是飞行器的重要组成部分，为飞行控制系统提供高度和速度等重要的信息源。
The control system automatically regulates the buoyancy force of the gasbag according to parameters of a sensor, so as to achieve the gravity balance and energy-saving flight of the whole aircraft.
控制系统根据传感器参数自动调节气囊的浮升力，达到整机的重力平衡和节能飞行。
The control system automatically regulates the buoyancy force of the gasbag according to parameters of a sensor, so as to achieve the gravity balance and energy-saving flight of the whole aircraft.
控制系统根据传感器参数自动调节气囊的浮升力，达到整机的重力平衡和节能飞行。
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