这两种方法成功地用于直升机飞控系统的设计。
The method has been applied to design of a helicopter flight control system.
指出了未来可重构飞控系统的实现途径和发展趋势。
Implement ways and development trends for the future reconfigurable flight control system are pointed out.
传统的飞控系统设计技术很难满足品质设计的要求。
Conventional technology of PCS design cannot meet the requirements for quality design.
指出了未来可重构飞控系统的实现途径和发展趋势。
Implement ways and development trends for the future reconfigurable flight control system a...
这是我国首次将单片计算机应用到无人机的飞控系统。
This is the first time in our country that an autopilot equipped in a domestic target plane employs single-chip microcomputers.
讨论了可重构飞控系统的故障可检测性、可重构性等基本概念。
The conception of failure detectability and reconfiguration are discussed for reconfigurable control system.
本文主要研究了集成式无人机飞控系统开发平台设计的相关技术。
This thesis studies the integrate flight control design platform applied in unmanned aircraft control systems.
通过对飞控系统各项功能与特点的检验，对飞控系统简化模型进行了验证。
The simplified model is validated by verifying the main characteristics and functions of the FCS.
J - 10采用了611所研究的数字4余度(4个通道)电传飞控系统。
The J-10 USES a digital quadruplex four-channel FBW system developed by the 611 Institute.
针对飞控系统故障诊断，提出了一种利用动态信息对故障进行检测的新方法。
Aiming at fault detection of flight control system, the article presents a new method of fault detection using dynamic data.
提出了在几种主要因素影响下进行飞控系统性能和可靠性一体化分析的方法。
This paper proposes an approach of integrated analysis of performance and reliability for missile's flight control system under the effects of some important factors.
本文从总体设计的角度，对飞控系统控制律设计与评估方法进行了初步的探讨。
The work present here is the designing and evaluating techniques of Flight Control Law (FCL) from the point of view of conceptual aircraft design.
霍尼韦尔提供电传飞控系统，惯性参考和空中数据系统，辅助动力装置，机轮刹车。
Honeywell Providing fly-by-wire flight control system, inertial reference and air data systems, auxiliary power unit, wheels and brakes.
飞机飞控系统的寿命周期费用估算与预测是航空工程系统优化和研发的重要环节。
The evaluation and forecast of the life cycle cost for an aircraft flight system is the important link in the system optimization and R&D of aviation engineering.
同时还介绍了一单通道主飞控系统的地面演示和一副翼配平控制系统的飞行演示。
The paper also describes a ground demonstration of a one channel primary flight control system and a flight demonstration of an aileron trim control system.
最后着重说明了某机载ACT飞控系统15 5 3B总线通信网络的实现技术。
The implement technique of 1553B bus communication network in airborne ACT flight control system is presented stressfully.
针对复杂的飞控系统传感器故障类型，建立了故障诊断模型，提取了各种故障数据。
Aimed at complex sensors faults of aircraft control system, the fault diagnosis models are set up and various fault data are acquired.
本文首先介绍了无人机飞控系统的设计过程，采用模型飞行试验进行控制律参数设置与确定。
Firstly, the paper introduce the process of design the UAV AFCS, which use the test of model fly to confirm the control principle parameter.
该飞控系统内建标记了诸如监狱发电厂等无人机飞行不存在问题但其所载物品是否违禁的区域。
The system has built-in restrictions around sensitive locations such as prisons and power plants, where potential payloads, not the flying itself, are a concern.
其次，文中对设计的飞控系统进行了稳定性分析，提出阻尼器与增稳控制系统相融合的控制方式。
Secondly, the stability of designed AFCS is analyzed and an amalgamation control mode of damper and stability augmentation control system is put forward in the paper.
并对实现这两种飞行控制系统所要研究的具体技术进行了阐述，为新一代飞控系统设计提供了参考。
And relative technologies for achieving the two flight control systems are discussed. A design reference is provided to develop a new flight control 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。
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.
文中首先采用反馈线性化理论设计了非线性飞控系统，进一步设计了非线性飞控系统仿真视景演示平台。
In the paper, the application of feedback linearization in the flight control is described firstly, then the simulation demo system of nonlinear flight control system is designed.
为建立合理的飞机飞控系统液压作动器的虚拟样机，必须对其关键部件密封圈的受力状况进行计算分析。
In order to establish a reasonable virtual prototype for the hydraulic actuators ot aircraft Ihght control system, the stress state of the key components, the sealing ring must be calculated.
在综述虚拟原型技术的基础上，研究飞行控制系统虚拟原型机以及采用虚拟原型技术后飞控系统的设计方法。
Based on the survey of virtual prototyping technology, the design method of flight control systems by using virtual prototyping technology is studied.
根据无人机飞控系统的特点及其智能故障诊断的需求，采用专家系统技术设计无人机飞行控制系统的故障诊断。
According to the characteristics of UAV flight control system and requirements of fault diagnosis, it used expert systems approach to design the fault diagnosis of UAV flight control system.
介绍了一种自动飞控系统(AFCS)测试系统的设计和实现，对其中主要硬件的设计和上层测试软件的设计思想做了讨论。
Design of an automatic test system for automatic flight control system (AFCS) is presented. The development of major hardware and the design ideas of test software are discussed.
介绍了一种自动飞控系统(AFCS)测试系统的设计和实现，对其中主要硬件的设计和上层测试软件的设计思想做了讨论。
Design of an automatic test system for automatic flight control system (AFCS) is presented. The development of major hardware and the design ideas of test software are discussed.
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