通过此协议，插线单元之间可直接进行信息交换，以便为插线系统互锁建立简单无人控制系统。
By means of this protocol informa"-tion can also be exchanged directly between bay units so as to set up simple masterless systems for bay and system interlocking ."
该系统还可以与其他系统同时跟踪，诸如无人机和航空控制系统。
The system can also track in parallel with other systems, such as drones and air control units.
例如，作为“英国宇航系统公司”计划之一的无人机联合控制系统将使得喷气式飞机的飞行员在飞行过程中同时指派无人机分队执行侦查或战斗任务。
Among BAE Systems’ plans, for example, is the co-operative control of drones, which would allow a pilot in a jet to fly with a squadron of the robot aircraft on surveillance or combat missions.
有关机构也将研究操作和安全问题，将无人驾驶飞行器与当前的空中交通控制系统整合在一起。
The agency also will investigate the operation and safetyissues associated with integrating unpiloted aircraft into today's air trafficcontrol system.
一旦通过“恶魔”无人机的试验收集到足够的数据，可能要么是制造一架更大的试验飞机，要么就是改装一架现有的飞机，并在这架飞机上进行射流控制系统的试验。
Once enough data have been gathered from demon, either a larger demonstration aircraft will be built or the technology will be tested by converting an existing plane.
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.
本文把该方法应用于无人直升机，给出了自适应姿态控制系统和跟踪控制器的设计方法。
This method is applied to an unmanned helicopter, and the design of an adaptive attitude controller and a trajectory-tracking controller are presented.
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.
在本篇论文的最后，就微型无人直升机控制系统设计中存在的问题做了一定的探讨和展望。
In the end, some exploration and prospect about problems of flight control system design for autonomous miniature helicopter are presented.
本文介绍“长空”超低空无人驾驶飞机的飞行控制系统。
The paper introduces the flight control system of the pilotless aircraft.
现代无人直升机飞行控制系统一般由飞行控制计算机、伺服驱动机构、传感器、地面监测控制等分系统组成。
The modern unmanned helicopter flight control system is generally composed of the flight control computer, the servo driving mechanism, the sensor, and the ground monitor control system etc.
遥控系统是无人驾驶直升机控制系统的主要组成部分。
Telecontrol system is the most primary part of unmanned helicopter control system.
该文分析了无人直升机飞行控制系统软件实现要求。
The requirements of software implementation for unmanned helicopter flight control system are analyzed in the paper.
然后对高稳定性无人机飞行控制系统进行了系统原理分析和控制律原理分析，提出了设计任务以及应遵循的主要设计原则。
After that a control system of the unmanned helicopter in high stability was analyzed with the system principle and control law, with which the design task and its design rule was proposed.
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.
本文介绍了某型无人驾驶飞机系列MCS - 51单片机控制系统的软件容错设计方法与实现。
This paper presents a fault-tolerant software design method and its application to the micro-controller system (MCS-51) of a type of Pilotless aircraft.
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).
针对传统无人机导航控制的局限性，提出基于多模变结构智能控制策略的导航控制系统。
Due to the limit of traditional UAV navigation control, this paper puts forward a kind of navigation control system that is based on the strategy of multi-model variable structure intelligent control.
将神经网络与专家系统相结合，提出了一种应用于无人机指挥控制系统的智能故障诊断方法。
An intelligent fault diagnosis approach for UAV command and control system is presented by combining neural network and expert system.
第2章介绍了无人直升机飞行控制特点、任务以及飞行控制系统方案。
In Chapter 2, the scheme of the mini unmanned helicopter's flight control system is presented based on understanding its characteristic and mission.
针对飞翼无人机的特性，利用侧航法和侧滑法设计了侧风着陆控制系统，仿真了系统抗侧风干扰的能力并进行了对比分析。
Based on the characteristics of flying wing UAVs, crosswind landing control systems were designed through the crabbed method and the side-slipping method.
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。
DMC-PID bunches control technology in the Angle of attack automatic control system during unpowered flying automatic landing period is introduced.
无人机系统是一个“人在回路”的复杂控制系统。
The UAV (Unmanned Air Vehicles) system is a complicated control system of man-in-the-loop.
采用非相似余度设计思想，建立了无人机横侧向控制系统。
With the method of dissimilar redundant design, this paper put forwards a lateral direction control system of UAV.
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。
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.
提出了一种基于可编程片上系统(SOPC)技术的无人机飞行控制系统硬件解决方案。
This paper introduces a solution to satisfy the need of the hardware platform for the UAVs based on the System on a Programmable Chip (SOPC) technology.
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.
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.
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