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相关概念视频

Linear Approximation in Time Domain01:21

Linear Approximation in Time Domain

72
Nonlinear systems often require sophisticated approaches for accurate modeling and analysis, with state-space representation being particularly effective. This method is especially useful for systems where variables and parameters vary with time or operating conditions, such as in a simple pendulum or a translational mechanical system with nonlinear springs.
For a simple pendulum with a mass evenly distributed along its length and the center of mass located at half the pendulum's length,...
72
Time-Domain Interpretation of PD Control01:07

Time-Domain Interpretation of PD Control

85
Proportional-Derivative (PD) control is a widely used control method in various engineering systems to enhance stability and performance. In a system with only proportional control, common issues include high maximum overshoot and oscillation, observed in both the error signal and its rate of change. This behavior can be divided into three distinct phases: initial overshoot, subsequent undershoot, and gradual stabilization.
Consider the example of control of motor torque. Initially, a positive...
85
Relative Motion Analysis using Rotating Axes-Problem Solving01:29

Relative Motion Analysis using Rotating Axes-Problem Solving

394
Consider a crane whose telescopic boom rotates with an angular velocity of 0.04 rad/s and angular acceleration of 0.02 rad/s2. Along with the rotation, the boom also extends linearly with a uniform speed of 5 m/s. The extension of the boom is measured at point D, which is measured with respect to the fixed point C on the other end of the boom. For the given instant, the distance between points C and D is 60 meters.
Here, in order to determine the magnitude of velocity and acceleration for point...
394
Relative Motion Analysis using Rotating Axes01:25

Relative Motion Analysis using Rotating Axes

450
Consider a component AB undergoing a linear motion. Along with a linear motion, point B also rotates around point A. To comprehend this complex movement, position vectors for both points A and B are established using a stationary reference frame.
However, to express the relative position of point B relative to point A, an additional frame of reference, denoted as x'y', is necessary. This additional frame not only translates but also rotates relative to the fixed frame, making it...
450
Feedback control systems01:26

Feedback control systems

296
Feedback control systems are categorized in various ways based on their design, analysis, and signal types.
Linear feedback systems are theoretical models that simplify analysis and design. These systems operate under the principle that their output is directly proportional to their input within certain ranges. For instance, an amplifier in a control system behaves linearly as long as the input signal remains within a specific range. However, most physical systems exhibit inherent nonlinearity...
296
Absolute Motion Analysis- General Plane Motion01:24

Absolute Motion Analysis- General Plane Motion

218
Visualize a drone, with its propellers spinning rapidly, hovering mid-air. The fascinating movements and operations of this drone can be comprehended by applying the principle of general plane motion.
As the drone's propellers rotate, an upward force is generated that counteracts the force of gravity, enabling the drone to lift off from the ground. This initial movement of the drone is along a straight path, representing a form of translational motion. In this phase, every point on the...
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Updated: Jun 14, 2025

Gain-compensation Methodology for a Sinusoidal Scan of a Galvanometer Mirror in Proportional-Integral-Differential Control Using Pre-emphasis Techniques
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增强预定义时间控制用于航天器态度跟踪:一种动态预测方法.

Jinhe Yang1,2, Tongjian Guo1, Yi Yu1

  • 1Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, China.

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概括

这项研究引入了航天器态度跟踪的新控制策略,在设定的时间限制内实现高精度. 该方法提高了稳定性,并使用先进的预测算法减少了错误.

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态度跟踪 态度跟踪跟踪动态预测技术 动态预测技术预定义的时间控制控制器.刚性太空飞船 刚性太空飞船最快的更新预测期预测期.

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科学领域:

  • 航空航天工程 航空航天工程
  • 控制系统理论 控制系统理论
  • 机器人技术 机器人技术 机器人技术

背景情况:

  • 太空飞船的态度控制对于任务的成功至关重要.
  • 现有的控制方法经常与不确定性和干扰作斗争.
  • 预定义的时间控制提供了有限时间的融合,但可以是限制性的.

研究的目的:

  • 开发一个强大的预定义时间控制战略,用于固定的航天器态度跟踪.
  • 有效地减轻系统不确定性和环境干扰.
  • 为了放松预定义时间控制中的限制性条件,并简化参数调整.

主要方法:

  • 使用动态预测技术进行态度跟踪.
  • 实施先进的预测算法来处理不确定性.
  • 使用终端滑动模式控制和预测方法开发一个连续的,强大的控制规律.
  • 为期更新引入自适应性全球优化.

主要成果:

  • 在预先定义的时间限制内实现了强大而精确的态度跟踪.
  • 成功缓解了系统不确定性和环境干扰.
  • 在稳定状态下,降低态度跟踪误差到不到0.01度.
  • 证明了更容易的参数调整和系统稳定性的非保守的上限.

结论:

  • 拟议的预定义时间控制策略对于刚性航天器态度跟踪是有效的.
  • 预测方法和终端滑动模式控制的整合提高了稳定性和精度.
  • 适应性全球优化方法缓解了预定义时间控制中的先前限制.