attitude control system发音

意思翻译

姿态控制系统

相似词语短语

control system───操纵系统; 控制设备; 控制系统; 控制制度；[自]控制系统

executive control system───[计]执行控制系统

attitude───n.态度；看法；意见；姿势

furnishes attitude───提供态度

attitude to───vt.对...态度，看法

censorious attitude───挑剔的态度

anachronous attitude───不合时宜的态度

businesslike attitude───公事公办的态度

control───v.指挥; 控制; 限定; 限制; 阻止蔓延; 抑制；n.统治; 控制（力）; 克制; 管理; 限制; 控制按钮; 检查站/人员; 对照标准；n.控制；管理；抑制；操纵装置；vt.控制；管理；抑制

双语使用场景

The algorithm has been embedded in the attitude control system of a small unmanned helicopter.───该算法已应用于小型无人直升机的姿态控制中。

As an application example, its application to flight attitude control system is analysed.───作为应用实例，分析了在飞行姿态控制系统中的应用。

integrated power and attitude control for a bias momentum attitude control system is investigated.───研究偏置动量姿态控制系统中的集成能量与姿态控制问题。

One of the difficult techniques of a remote sensing satellite is to make its attitude control system to a certain accuracy.───地球遥感卫星的技术难点之一是保持有足够的姿态控制精度。

The control law of the flywheel in an integrated power and attitude control system (IPACS) for a spacecraft is investigated.───研究航天器集成能量与姿态控制系统中飞轮的控制律。

Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.───反作用轮是影响航天器姿态控制系统精度的主要扰动源之一。

Flywheel has been identified as one of the main disturbance sources that affect the precision of attitude control system of spacecraft.───飞轮是高精度航天器姿态控制的主要干扰源之一。

This article deals with torque allocation for redundant flywheel configurations in a spacecraft attitude control system.───主要研究了航天器姿控系统中冗余飞轮构型的力矩分配问题。

Attitude control system design, guidance system accuracy analysis and load calculation of rocket have close relationship with wind field.───风场的应用涉及运载火箭姿态控制系统设计、制导精度分析和载荷分析计算等多方面的工作。

英语使用场景

The three axis stabilized Earth oriented attitude control system adopted by FY 1 meteorological satellites represents an active control concept.

Microwave phase shifter in phased-array radar, communications, instrumentation, heavy ion accelerator and the missile attitude control system has a broad application prospects.

The application of gravity gradient in the attitude control system of mini-satellites provides an advantaged tool for the development and research of the miniaturization of satellites.

In order to improve the pointing accuracy of small satellite, the attitude control system is controlled with pitch-axis momentum and three-axis magnetic torque.

A nonlinear attitude control system was designed by choosing a nonlinear system tracing a linear reference model system, based on model reference variable structure control method.

The suspension damping control strategy for vehicle attitude control system is presented.

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.

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.

The fault simulation of satellite attitude control system is crucial for research and experimental verification on optimizing configuration, fault diagnosis, reconstruction of control system.