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- Triplex Flight Control System 三重飞行控制系统
- Subsystems of flight control system II. 飞行控制系统的分系统2。
- The design of the flight control system with the vectored thrust is discussed. 对带推力矢量飞机的飞控设计问题进行了研究。
- And during this case, flight control system (FCS) plays a more important role . 在上述改进的基础上,飞行控制系统起到关键性的作用。
- Missile rudders are executive bodies of missile flight control system. 舵机测试系统是导弹生产线上的重要设备。
- ALTITUDE ACQUIRE, A digital flight control system mode to transition from climb (or descend) to level flight. 高度截获,一种数字式飞行操纵系统,从爬升(或下降)改平的模式。
- That defect could cause solders to crack and the flight control system to fail, Ernst explains. 他拒绝提供细节，他的观点是，假零件肯定会导致严重事故。
- A new approach based on LPV model to design large envelope flight control system is presented. 介绍一种基于线性参变模型(LPV)设计大包线飞行控制器的新方法。
- Abstract: The design of the flight control system with the vectored thrust is discussed. 文摘:对带推力矢量飞机的飞控设计问题进行了研究。
- Abstract： The design of the flight control system with the vectored thrust is discussed. 摘 要： 对带推力矢量飞机的飞控设计问题进行了研究。
- The research emphasis of flight control system of UAH is to determine the flight states of UAH by use of measured data. 利用有限的测量数据来确定无人直升机的飞行状态变量是无人直升机飞行控制系统研究的热点。
- The flight control system can record 8 different flight paths and separate paths can be grouped to build new path. 飞行控制系统可记录8个不同的飞行路径动作，且可以将单个飞行路径组合起来形成新的飞行路径。
- Multi-loop feedback control was employed for underactuated flight control system of unmanned helicopter. 摘要针对无人直升机欠驱动特性，采用多回路反馈方法设计飞行控制系统。
- AUTOMATIC FLIGHT CONTROL SYSTEM, A system composed of all necessary subsystems needed to guide the flight of an airplane. 自动飞行控制系统,由所有能引导飞机飞行的子系统所组成的一个系统。
- Because these wind loads are a major structural consideration, they greatly influence the design of the flight control system. 因为这些风载荷是结构上主要的考虑因素，它们很大地影响着飞行控制系统的设计。
- A new inner/outer loop structure is proposed, and its application to the design of helicopter flight control system is described. 提出了一种新型的内／外回路控制结构，系统地阐述了此结构在直升机控制系统中的应用。
- Another aerodynamic improvement is the Digital Flight Control System, which improves the aircraft's reliability and reduces airframe weight. 另一个改进是气动数字飞行控制系统，提高了飞机的可靠性和降低了机身重量。
- The distributed flight control system is designed by using the ACE ORB (TAO) middleware and its event service mechanism. 摘要利用中间件TAO及其事件服务机制，设计了分布式飞行控制系统。
- The part two discusses some issues that relate to the design and construction of the redundant Digital Flight Control System(DFCS). 第二部分讨论了多余度数字式飞行控制系统设计和实现时的几个问题 。
- The simulation results show that designed flight control system can complete required maneuvering flight and possesses excellent tracking performance. 仿真结果表明:采用文中提出的设计方案,所设计的飞行控制系统能够完成要求的机动飞行动作并且具有优良的跟踪性能。
