attitude control system的意思

attitude control system中文翻譯：

姿態控制系統

相似詞語短語

control system───操縱系統; 控制設備; 控制系統; 控制制度；[自]控制系統

executive control system───[計]執行控制系統

attitude───n.態度；看法；意見；姿勢

furnishes attitude───提供態度

attitude to───vt.對...態度，看法

censorious attitude───挑剔的態度

anachronous attitude───不合時宜的態度

businesslike attitude───公事公辦的態度

control───v.指揮; 控制; 限定; 限制; 阻止蔓延; 抑制；n.統治; 控制（力）; 克制; 管理; 限制; 控制按鈕; 檢查站/人員; 對照標準；n.控制；管理；抑制；操縱裝置；vt.控制；管理；抑制

雙語使用場景

The algorithm has been embedded in the attitude control system of a small unmanned helicopter.───該算法已應用于小型無人直升機的姿態控制中。

As an application example, its application to flight attitude control system is analysed.───作為應用實例，分析了在飛行姿態控制系統中的應用。

integrated power and attitude control for a bias momentum attitude control system is investigated.───研究偏置動量姿態控制系統中的集成能量與姿態控制問題。

One of the difficult techniques of a remote sensing satellite is to make its attitude control system to a certain accuracy.───地球遙感衛星的技術難點之一是保持有足夠的姿態控制精度。

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與姿態控制系統中飛輪的控制律。

Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.───反作用輪是影響航天器姿態控制系統精度的主要擾動源之一。

Flywheel has been identified as one of the main disturbance sources that affect the precision of attitude control system of spacecraft.───飛輪是高精度航天器姿態控制的主要干擾源之一。

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統中冗余飛輪構型的力矩分配問題。

Attitude control system design, guidance system accuracy analysis and load calculation of rocket have close relationship with wind field.───風場的應用涉及運載火箭姿態控制系統設計、制導精度分析和載荷分析計算等多方面的工作。

英語使用場景

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.