The device comprises the vehicle-mounted response recognition system (1) which is connected with the navigation flying control system (4) of the unmanned plane.
其装置包括机载应答识别系统（1），机载应答识别系统与无人机上的导航飞行控制系统（4）连接。
This paper discusses the control instruction system with regard to the flying object.
本文论述一种飞行目标的控制指令系统。
The autonomous manipulation system control architecture of multi free flying space robots was discussed.
阐述了多个自由飞行空间机器人协调操作自主控制系统的控制结构。
For nonlinear attitude system of flying vehicle with pure time-delay, inertia and bang-bang control a control method using decoupling variable structure is given.
对于具有纯延迟、惯性和由开关控制的非线性飞行器姿态系统，本文提出了采用解耦变结构控制的方法。
DMC-PID bunches control technology in the Angle of attack automatic control system during unpowered flying automatic landing period is introduced.
介绍了将DMC - PID串级控制技术应用到无人机无动力飞行时的自动着陆阶段迎角自动控制系统。
Therefore, research for control strategies of flying simulating system and designing reasonable controller have the very important meaning.
因此深入研究飞行模拟系统控制策略，设计出合理的控制器具有极其重要的意义。
In order to simulate liner CCD remote sensor flying image and check up its image effect in laboratory, one kind of liner CCD remote sensor uniaxial turntable control system was designed.
为了在实验室条件下模拟线阵CCD遥感器的飞行成像，并验证其成像效果，设计了一种线阵CCD遥感器单轴转台控制系统。
The response characteristic of moving-mass control for the low-altitude aircraft is researched based on the moving-mass control system model of the flying saucer.
在建立碟形飞行器变质量矩控制数学模型的基础上，对低空飞行器变质量矩控制的响应特性进行了仿真研究。
The results show that the stability and control are sufficient, that the flying qualities are satisfactory after stability augmentation, and that the roll attitude protection system works as expected.
结果表明，稳定和控制是足够的，飞行品质满意后稳定性增强，滚动姿态保护系统的工作原理。
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。
Applying this method in the design of control system of a certain flying vehicle, the performance is significantly improved.
文中应用这种方法对某型飞行器控制系统进行了设计，使飞行器性能指标得到了显著提高。
In this paper, we discuss the optimal control problem for an elastic oscillating system of fine-long cube flying object with structure damping coefficient.
本文讨论具结构阻尼系数的细长体飞行器的弹性振动方程支配系统的最优控制问题。
In the control system of welded tube flying saw, it has higher controlling precision, stable running property and higher reliability.
介绍了新型焊管定尺飞锯计算机系统柔性控制、定尺精度的在线调整和可靠性设计。
The flying saucer is a certain statically unstable system, and with the model bias, the conventionally designed predictive control system is hard to get ideal control effect.
碟形飞行器是一类较为特别的静不稳定系统，在系统数学模型存在较大偏差的情况下，常规的预测控制设计思路难以获得理想控制效果。
The simulation and application show that the adaptive PID controller has better control performance than the ordinary PID controller in the flying shear control system.
仿真和应用结果表明，这种模糊自适应PID比常规PID控制器在飞剪控制中具有更好的控制性能。
Finally, main methods and characteristics of flying-wing UAV's control system design are analyzed based on nonlinear simulation results and some advice for improvement is presented.
最后，根据仿真结果分析总结了飞翼布局无人机的控制系统设计方法和设计特点，并提出一些具体的建议，为飞翼无人机总体设计提供了一定的依据。
This control system can provide automatic flying object tracking and measuring in visible and infrared band. It also can provide real-time output of the measured results.
该系统可以在可见和红外波段对飞行目标进行跟踪测量，还可对测量结果实时输出。
The studies of flying qualities during approach to landing for the fly—by—wire aircraft with control and augmented system were conducted on a fixed—base flying quality simulator in this paper.
针对电传控制增稳飞机进行了进场着陆的飞行品质地面模拟试验研究。
Based on the analysis of lateral-directional control system of a certain plane, representative fault infecting flying security is specialized;
在对某型飞机横向操纵系统分析基础上，列举出危害飞行安全的典型故障；
In reference to the model uncoupling part, it has been proved by the report of flying test. The structure of equivalent linear model have been demonstrated by the experiment of a control system.
本文的模型解耦部分得到空测报告的证明、等效线性模型结构在某型操纵系统试验中得到证实。
In reference to the model uncoupling part, it has been proved by the report of flying test. The structure of equivalent linear model have been demonstrated by the experiment of a control system.
本文的模型解耦部分得到空测报告的证明、等效线性模型结构在某型操纵系统试验中得到证实。
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