飞机舵机系统的机械故障可用解析余度法检测。
Aircraft actuator system failure can be detected by analytic redundancy analysis.
讨论了磁通综合式余度舵机系统电流均衡的设计问题。
The current equalization design of a redundant actuation system with magnetic flux sum is discussed.
进而确定舵机系统模型结构和相关参数，完成了控制器的设计。
The control actuator system model structure and related parameters are determined, and the controller is designed.
本文通过对舵机系统的组成部件的分析，叙述测控系统的工作原理。
This paper narrates the working principle of the control test system by analyzing the components of the rudder system.
本文的研究结论为工程中对电动舵机系统的故障诊断提供了重要参考。
The research results of this paper provide the important references to the fault detection of electro-mechanical actuator system in engineering.
同时介绍了弹用电动舵机系统的工作原理和TM 320lf 2407 A芯片的特点以及无刷直流电机在电动导弹舵机系统中的应用。
It presents the principle of the system of electrical vane mechanism in mis - sile and the feature of the chip TM320LF2407A, and the apply of BLDCM in the system of electrical vane mechanism.
舵机管路系统的投油清洗。
它是地面半实物仿真系统中的一种重要专用设备，用来模拟飞行器舵机在飞行过程中所承受空气动力力矩载荷。
It is an important half hardware-in-loop simulation equipment, which is often used to simulate the aerodynamic torque load on the missile rudder or elevon actuators in the flight.
舵机(锚机、绞缆机)液压系统安全装置调整。
Adjusting safety device for hydraulic system of steering gear (windlass, mooring winch).
以TMS320F2812作为主控CPU，以IR2110作为驱动芯片，完成了导弹舵机伺服控制系统的硬件设计，进行了控制器主电路的分析与设计。
The missile rudder servo controller adopts TMS320F2812 as main CPU, IR2110 as drive chip. Each part of main circuit is analyzed in detail.
对船用舵机泵控系统中位置控制单元的三通阀控制非对称缸和四通阀控制对称缸的两种设计方案进行了理论分析和系统结构分析。
Two design strategies that three-way valve control unsymmetrical cylinder and four way valve control symmetrical cylinder were analyzed from principle and system structure aspects.
以传统的舵机伺服系统动压反馈回路为基础，介绍了一种新的伺服系统动态校正方法。
In this paper, a new dynamic correcting way based on the traditional dynamic pressure feedback for the rudder servo system is proposed.
文章针对自动操舵仪测试系统自动控制部分的特点，结合舵机试验的特殊要求，说明了系统的整体设计思想与实现过程。
Contraposing the feature and the special demand of autocontrol section in automatic rudder experiment sys-tem, this paper illustrates its general method of designing and process of implementation.
首先给出了现有舵机的简化模型，深入分析了原有动压反馈回路对系统的作用影响。
At first this paper introduces the simplified rudder servo-system model and analyzes the influence of the dynamic pressure feedback on servo system.
电液控制单元是船用舵机电液位置伺服系统关键部件，其性能的优劣直接影响舵机的性能。
Electrohydraulic control unit whose performance has direct effect on rudder's characteristics is the key component of ship rudder position control system.
本课题以某型舵机控制器为研究对象，设计了一种数字控制液压伺服回路校准的软件实现方法，提高了系统的可靠性和可维护性。
Aimed at a kind of wing control system, a software method that digital control hydraulic servo circuits were calibrated was proposed to improve system's reliability and maintainability.
针对典型的舵机壳体类零件，在UGII平台上构造了一种交互式、智能化的计算机辅助工艺设计系统模型。
This paper focuses on typical actuator housing for airborne equipment. Aninteractive and intelligent computer aided process planning system model is constructed on UGII platform.
电动舵机是一个复杂的机电一体化系统。
The electric actuator is a complex electro-mechanization system.
本文针对电动舵机动态加载系统的控制策略进行了研究与设计。
In this paper, a control method aiming at electric actuator hydraulic loading system is discussed and designed.
结果表明，进行PI校正后的系统能够较好地满足舵机的稳定性和快速性要求，且工程中易于实现。
It is shown from practice that after PI correction the system can meet stability and fast response requirements of rudder machine, and it is easy to realize in the project.
某型四余度电液舵机是飞机平尾操纵系统的关键部件，是机、电、液高度耦合的复杂系统。
One four redundant steering engines is a crucial component of aircraft stabilizer manipulative systems, and it is a complicated system related to mechanical, electrical and hydraulic elements.
研究了舵机加载系统的变结构控制问题。
The application of variable structure control to the actuator load system was studied.
简要阐述了下位机软件实现对舵机电动加载系统实时控制的策略。
Strategy that control software control electric load system real-timely is discussed simply.
MCU采用PID算法，对小车的舵机转向角度及行进速度进行实时控制，实现了整个系统的双闭环控制。
MCU USES the PID algorithm, Real-time control of the vehicle steering Angle of the steering gear and road speed. At last, implementation of the entire system of double-loop control is introduced.
本文对高空超音速飞机中与增稳舵机交联的纵向机械操纵系统的力反传问题作了理论探讨。
This paper presents a. preliminary research on the feedback of feel of longitudinal mechanical control system connected with steering-engine in supersonic fighter.
舵机是机器人、机电系统和航模的重要执行机构。舵机控制器为舵机提供必要的能源和控制信号。
Servo motor is an important executive structure in robots, mechanism and electronics and (aeromodellings.) Servomotor controller supplies necessary power and control signals.
分析了数字舵机控制系统白勺控制过程、构造组成、硬件软件实现方案。
It analyzes the digital servo control system to control the process, structure, hardware and software implementations.
系统测试结果表明，该试验器能够满足舵机地面测试的功能及技术指标要求，其研究技术还可用于其他驱动场合。
Testing results of system show the tester meets the needs of function and demand in ground testing of actuator. The studying technology of the paper is also used to other drive situations.
系统测试结果表明，该试验器能够满足舵机地面测试的功能及技术指标要求，其研究技术还可用于其他驱动场合。
Testing results of system show the tester meets the needs of function and demand in ground testing of actuator. The studying technology of the paper is also used to other drive situations.
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