研究了上肢康复机器人的姿态控制问题。
The posture control of the rehabilitation robot for the human arm is investigated.
该算法已应用于小型无人直升机的姿态控制中。
The algorithm has been embedded in the attitude control system of a small unmanned helicopter.
研究了刚体飞行器大角度机动的姿态控制问题。
In this paper, attitude control problem of a rigid spacecraft with large Angle maneuvers is investigated.
提出了一种基于神经网络扰动补偿的姿态控制方法。
This paper presents a control scheme based on NN disturbance compensation for attitude control of satellite.
针对单轴定向大气层外拦截器设计了一种姿态控制律。
An attitude control law for single axial direction control of an exoatmospheric interceptor is put forward.
系统中飞轮是姿态控制的执行机构，同时也是储能装置。
The flywheels are used as attitude control actuators as well as energy storage device.
通过卫星姿态控制的算例具体说明了这种优化设计过程。
The design procedure is demonstrated by a satellite attitude control example.
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.
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。
The integrated power and attitude control for a bias momentum attitude control system is investigated.
在人造卫星的姿态控制中，广泛地采用偏置动量轮控制系统。
A momentum wheel control system is widely used for the attitude control of satellite.
针对俯仰回路，利用测量的俯仰角实现了俯仰回路姿态控制；
The pitch control is attained by the measurement of the pitch angle.
对航天器姿态动力学模型和姿态控制技术进行了概括和总结。
The model of spacecraft attitude dynamics and the attitude control technology are generalized.
研究了基于偏航观测器的三轴稳定偏置动量对地定向卫星姿态控制问题。
Attitude control problem of a three-axis stabilized, momentum biased, and nadir-pointing satellite is investigated based on yaw observer.
卫星姿态动力学系统与其线性化模型之间的误差会影响姿态控制的精度。
The error between satellite attitude dynamics and its linearized model can affect the attitude control precision.
该算法可用于曲面加工过程中的刀具姿态控制，以避免曲面的过切现象。
The algorithm can be used to control the orientation of the cutter so as to avoid over-cutting in surface machining.
姿态控制发动机真空环境下工作产生的羽流对航天器造成的影响非常明显。
The plume from the attitude controlling rocket motor nozzle has an obvious effect on the aircraft in vacuum.
本文利用整体微分几何的方法研究了人造卫星的轨道控制和姿态控制问题。
The orbit control and attitude control problems of satellite have been studied in this thesis by use of global differential geometry method.
直接侧向力控制分为轨迹控制与姿态控制两种方式，本文研究姿态直接力控制。
The direct lateral force control includes two ways: trajectory control and position control. This research aims at lateral force control.
根据软着陆不同阶段飞行任务的不同，分阶段提出了月球探测器的姿态控制方案。
According to the flight mission of the different phases, the attitude control schemes were designed in the paper respectively.
研究了最近提出的非线性自抗扰控制器在大挠性多体卫星姿态控制中的应用问题。
The recently developed nonlinear Active Disturbance Rejection Controller (ADRC) was applied to the attitude control of large flexible multi-body satellite with reaction wheels.
基于旋转群代数，以航天器姿态控制研究为背景，提出了四元数的核心矩阵的概念。
A concept of kernel matrix of quaternion is proposed, which is based on rotation group algebra and with spacecraft attitude control as its background.
讨论了其滑模面的构造方法和解耦控制条件，在姿态控制中保证了姿态跟踪期望值。
As to the attitude stablization of reentry vehicle with parameter uncertainties, its variable structure decoupling control law is designed and simulation results are given.
空间交会对接涉及到两个航天器同时要进行多达12个自由度的轨道和姿态控制问题。
The rendezvous and docking (RVD) between two spacecrafts in space involves both orbit control and attitude control with up to 12 degrees of freedom.
然后，基于某型小卫星的姿态控制问题，设计了高精度定向阶段的神经网络补偿控制器。
Then, base on the problem of attitude control of a satellite under development, we design a NN compensation controller for high accuracy orientation phase.
从盾构机制造及盾构施工隧道管片姿态控制的角度讲述了盾构隧道与设计线路隧道的关系。
The relation of shield tunnel and the designing tunnel is stated from the Angle of shield machine production and attitude control of the duct piece.
仿真结果表明：即使系统存在不确定性和外界干扰，仍可在闭环系统中实现精确的姿态控制。
Simulation results show that, in the closed-loop system, precise attitude control is accomplished in spite of the uncertainties and external disturbances in the system.
针对管道焊接机器人焊枪姿态控制问题，提出了一种基于专家系统的焊枪姿态智能控制系统。
To solve the problem of control to the welding torch 's gesture of pipeline welding robot, an intelligent control system of the torch' s gesture based on the expert system is presented.
由于采用的红外地平仪无法测量卫星的偏航信息，提出了一种基于偏航观测器的姿态控制方案。
Since the measurement of the yaw angle is unavailable by horizon sensor, an attitude control scheme of the satellite is proposed based on yaw observer.
由于采用的红外地平仪无法测量卫星的偏航信息，提出了一种基于偏航观测器的姿态控制方案。
Since the measurement of the yaw angle is unavailable by horizon sensor, an attitude control scheme of the satellite is proposed based on yaw observer.
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