如果数字计算机两次失败，飞行控制系统切换到模拟模式。
If two of the digital computers failed, the flight control system switched to the analog mode.
飞行控制系统设计是一项复杂的系统工程，涉及众多的专业。
As a complex system engineering, the design of flight control system is related to many specialties.
具有电传飞行控制系统的飞机，其飞行品质取决于系统参数。
The flying qualities of the aircraft with FBW FCS is determined by the varied parameters of the system.
本文围绕小型无人直升机飞行控制系统的设计与实现展开论述。
This paper focuses on the design and implementation of the flight control system for small unmanned helicopters.
本文围绕超小型无人直升机飞行控制系统的设计与实现展开论述。
This thesis focuses on the design and implementation of a flight control system for a mini unmanned helicopter.
飞行控制系统试图在周日前使不能工作的氨气泵重新工作，不过断路器跳闸了。
Flight controllers tried to restart the disabled ammonia pump early on Sunday but the circuit breaker tripped again.
本文主要进行了无人机自主编队飞行控制系统的设计方法及应用研究。
This dissertation mainly investigated the design and application of autonomous formation flight control system of unmanned aerial vehicles (UAVs).
本文概述了神经网络在飞行控制系统中的应用，并分析了应用中的困难。
This paper surveys the application of neural networks in flight control system, and analyzes the difficulties in application.
首先对平流层演示飞艇的自主飞行控制系统和遥测遥控系统进行了介绍；
Autonomous flight control system and telemetry and telecontrol system of stratospheric demonstration airship are introduced firstly.
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。
So making researches on the light aircraft flight control system is of theory, engineering and economical value.
利用非线性系统的扩展线性化方法设计具有大迎角的非线性飞行控制系统。
The extended linearization of nonlinear systems is used to design flight control systems at high angle of attack.
针对过失速机动飞机探讨了非线性动态逆方法在飞行控制系统设计中的应用。
This paper discussed the application of this method in the design of flight control system for the post stall maneuver.
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.
建立了驾驶员最优控制模型，提出了飞行控制系统优化设计目标函数和设计方法。
The pilot's optimal control model is investigated. The optimal design destination function and method of flight controlling system have been proposed.
并以法向过载控制模态为例，将线性二次型运用到飞行控制系统的控制律设计中。
The LQ is adapted to the flight control law design such as the Normal Acceleration 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。
Because these wind loads are a major structural consideration, they greatly influence the design of the flight control 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.
靶机驾驶员座舱内原来的飞行员座位移除提供额外的空间用于自动化飞行控制系统。
The target drone has the original pilot seat in the cockpit removed to provide additional space for the automated flight control system.
最后，用奇异摄动法具体设计了数字飞行控制系统（DFCS），并用微机予以实现。
Finally, the practical example design of the digital flight control system(DFCS) and DFCS microcomputer implementation are treated.
这是一个三轴自动飞行控制系统，它由模拟式的控制增稳系统和数字式自动驾驶仪组成。
It is a automatic flight control system for three axes, and consists of analog control augmentation system and digital autopilot.
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。
All the MH-60Gs have an automatic flight control system to stabilize the aircraft in typical flight altitudes.
研究了基于嵌入式微控制器LPC2138的空中机器人飞行控制系统的设计与实现技术。
The work focuses on an application and realization of embedded micro-controller LPC2138 in flight control system for aerial robotics.
自修复飞行控制是先进飞行控制系统的重要研究内容，它可以提高飞机的可靠性和生存能力。
The self-repairing flight control is one of the most important parts in advanced flight control system, and it can improve the reliability and viability of the plane.
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。
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.
飞机在飞行过程中，因某些测量元件出现故障致使信号丢失，会严重影响飞行控制系统的正常工作。
Some failing measuring components may lead the loss of signal, and work seriously on the flight control system during the flight.
根据无人直升机飞行控制特点，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。
According to the flight control characteristics for unmanned helicopter, we design distributed flight control system by means of using middleware TAO and its event service mechanism.
本文主要研究了闭环控制系统的故障检测和基于故障检测的自适应重构控制在飞行控制系统中的应用。
We mainly research on fault detection of closed-loop control systems and adaptive reconfiguration control based on fault detection and its application on flight control systems.
介绍了自动驾驶仪mp2000的原理及使用方法。并讨论了其在飞行控制系统中的应用与控制作用。
Introduce the principle of autopilot MP2000 and how to use it. Discuss its application in Aircraft-Control-System and its control effect.
考虑到飞行控制系统闭环反馈及实时的特性，设计了多个鲁棒自适应观测器用于传感器的故障隔离与重构。
Based on performance of real-time and closed loop feedback flight control system, a set of robust adaptive observers are set up for sensor fault isolation and reconfiguration.
考虑到飞行控制系统闭环反馈及实时的特性，设计了多个鲁棒自适应观测器用于传感器的故障隔离与重构。
Based on performance of real-time and closed loop feedback flight control system, a set of robust adaptive observers are set up for sensor fault isolation and reconfiguration.
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