介绍了变体飞行器控制系统和涉及的控制理论问题。
The control system and related control theory of morphing aircraft are introduced.
姿态控制推力器(act)是飞行器控制系统的执行部件。
The attitude control thruster (ACT) is the control component of the flight vehicle.
从时域内对存在模型误差的弹性飞行器控制系统进行了稳定鲁棒性研究。
The stability robustness for uncertain system models of elastic vehicles is studied in time-domain.
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。
Applying this method in the design of control system of a certain flying vehicle, the performance is significantly improved.
我们公司提供的这款遥控飞行器控制系统，结构灵活，控制系统可扩大，主要用于地面，海洋表面和高性能车辆等领域。
The Micro Systems, Inc MOdular Networked TArGet control Equipment (MONTAGE) is a flexible, expandable control system for ground, sea surface, and high performance air vehicles.
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.
Skylifter计划使用数个上述装置来控制飞行器的水平运动，并在表膜层内置浮力控制系统来调节垂直升降。
Skylifter plans to use several such drives to control the craft's horizontal motion and to aid a buoyancy-control system within the envelope in moving the vehicle up and down.
文中给出了一个弹性飞行器的姿态控制系统作为设计举例。
An example of an attitude control system of a bending vehicle is given.
目前空间飞行器的高精度姿态控制系统大多采用飞轮系统。
Now, flywheels systems are elected as the actuators of attitude control system with high precision for most spacecrafts.
星敏感器是为空间飞行器姿态控制系统提供姿态信息的测量系统。
The star sensor is a measuring unit used for providing information to the attitude control system on spacecraft .
例如在现代飞行器中，动力助推控制系统将飞行员的力放大以推动受到很大的气流作用的机翼表面。
In a modern aircraft, for example, the power boost controls amplify the force applied by the pilot to move the control surface against large aerodynamic forces.
在航空航天飞行器设计中，随着主动控制技术、随控布局及电传操纵系统的普遍采用，飞行控制系统的地位变得更为重要。
With widespread adopting of the Active Control Technique(ACT) and Control Configuration Vehicle(CCV)and Fly-by- wire system, position of Flight ControlSystem(FCS) become even more significant.
气动伺服弹性系统在不确定性摄动下的鲁棒稳定性问题对于带有自动控制系统的弹性飞行器是非常关键的。
Robust stability of the aeroservoelastic systems subjected to the perturbation of uncertainties is very important for elastic flight vehicles with automatic flight control systems.
基于奇异摄动思想，将飞行器姿态控制系统分为慢变化的姿态角回路和快变化的角速度回路分别设计。
The spacecraft's attitude control system was divided into the outer loop that was Angle loop and the inner loop that was Angle velocity loop based on their time scales.
基于时标分离思想，将飞行器姿态控制系统分为慢变化的姿态角回路和快变化的角速度回路分别设计。
The aerocraft's attitude control system is divided into the outer loop that is an Angle loop and the inner loop that is an Angle velocity loop based on their timescale separation principle.
本文介绍了以单片机系统来实现一个飞行器的控制系统，详细说明了其中的软件设计技巧。
The paper introduces a design to achieve the flyer's control system with a single chip computer and enter into details on the software design technique.
推导系统参数间的关系式，分析挠性空间飞行器主轴姿态控制系统稳定性问题。
The relation among parameters is derived and the stability of single axis flexible spacecraft attitude control system is studied.
同时为了实现初级的自主控制，考虑到飞行器的特点，设计了路径规划控制系统，使系统具有一定的程度的自主能力。
Finally, we design a path planner added to the autonomous control system to meet a certain extent of autonomous flight capability.
本文应用区间矩阵的理论，研究三轴稳定的挠性空间飞行器姿态控制系统的鲁棒稳定性分析问题。
In this paper, the robustness stability analysis of the attitude control system of a three-axis stabilized flexible spacecraft is investigated.
本发明还涉及安装有所述设备的飞行控制系统和包括所述系统的飞行器。
The present invention also relates to flight control systems in which said device is implemented and the aircraft comprising said systems.
大气数据测量系统是飞行器的重要组成部分，为飞行控制系统提供高度和速度等重要的信息源。
The atmosphere data measure system plays a very important role in an aircraft system and it provides the height and velocity information and so forth for the flight control system.
大气数据测量系统是飞行器的重要组成部分，为飞行控制系统提供高度和速度等重要的信息源。
The atmosphere data measure system plays a very important role in an aircraft system and it provides the height and velocity information and so forth for the flight control system.
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