基本释义:

执行机构，控制柜

网络释义

1)actuator cabinet,执行机构，控制柜

2)electric control actuator,电力控制执行机构

3)final control element,执行机构，末控元件，控制系统执行元件;(控制系统)执行元件

4)electrical control actuator,电控执行机构

5)attitude control actuator of spacecraft,航天器姿态控制执行机构

6)executive control,执行控制

用法和例句

A study of the prefrontal executive control of behavior and the electrophysiology in macaca mulatas;

恒河猴前额叶执行控制功能的行为和电生理研究

Task switching is a basic manner in human’s cognitive activities, and the switching process is an important aspect of executive control, it is considered as controlling switching course between two tasks which compete the same cognitive resources.

行为实验和神经生理学实验在转换加工的研究范式、转换代价的成分以及执行控制的理论等领域取得一定成果,但也存在诸多争议。

Task switching is an important paradigm in the study of executive control.

任务切换是当前研究执行控制的重要范式。

attitude control actuator of spacecraft

航天器姿态控制执行机构

Intelligent variable structure output feedback maneuvering control for flexible spacecraft

挠性航天器姿态机动智能变结构输出反馈控制

The Chaotic Attitude Control in the Large Angle Attitude Maneuver of Liquid-Filled Flexible Spacecraft

柔性充液航天器姿态转换机动及混沌姿态控制

Active Vibration Control of Flexible Spacecraft during Attitude Maneuver

挠性航天器姿态机动的主动振动控制

QUASI-EULER-ANGLES FEEDBACK CONTROL OF SPACECRAFT ATTITUDE MANEUVER

航天器姿态机动的拟欧拉角反馈控制

Research on Method of Spacecraft Attitude Control Based on Sliding Variable Structure

基于滑模变结构的航天器姿态控制方法研究

Study on the Minimal Energy Maneuvering Control of a Rigid Spacecraft with Momentum Transfer

刚体航天器的最小能量姿态机动最优控制研究

Adaptive Sliding Mode Control for Attitude Maneuvering of Flexible Spacecraft

挠性航天器姿态机动的自适应滑模控制

Attitude Controller Design for Combined Spacecraft after Separation

组合式航天器分离后姿态控制器设计

Research on Spacecraft Attitude Controller Based on DDFC

基于DDFC的航天器姿态控制器设计方法

Research on Normal Matrix Methodology of Attitude Control for Spacecraft

航天器姿态控制的正规矩阵方法研究

The Attitude Dynamics and Control of On-Orbit Refueling Spacecrafts

航天器在轨加注的姿态动力学与控制

Nonlinear control of attitude stabilization of an underactuated spacecraft

欠驱动航天器姿态稳定的非线性控制

Attitude Control of Spacecraft via Fliess Functional Expansion

基于Fliess泛函展开式的航天器姿态控制

Intelligent Adaptive Variable Structure Attitude Maneuvering Control for Flexible Spacecraft with Actuator Saturation

控制输入饱和的挠性航天器姿态机动智能鲁棒控制

Optimized design of controller parameters for large angle spacecraft attitude maneuvers

航天器大角度姿态快速机动控制器参数优化设计

Adaptive attitude control and active vibration control of the flexible spacecraft

一种挠性航天器的自适应姿态控制与振动控制

Design of higher-order sliding mode controller for rigid spacecraft attitude tracking maneuver

刚体航天器姿态跟踪的高阶滑模控制器设计