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相关概念视频

Circular Orbits and Critical Velocity for Satellites01:16

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The Moon orbits around the Earth. In turn, the Earth (and other planets) orbit the Sun. The space directly above our atmosphere is filled with artificial satellites in orbit. One can examine the circular orbit, the simplest kind of orbit, to understand the relationship between the speed and the period of planets and satellites with respect to their positions and the bodies that they orbit.
Nicolaus Copernicus (1473-1543) first suggested that the Earth and all other planets orbit the Sun in...
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Relative Motion Analysis using Rotating Axes-Problem Solving

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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...
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Azimuths and Bearings

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Azimuths and bearings are essential concepts in surveying, providing methods to express the direction of a line relative to a meridian. Azimuths refer to the clockwise angle measured from the north end of a reference meridian to the given line, ranging from zero to 360 degrees. This method gives a comprehensive directional reference within a full 360-degree circle, making it a straightforward way to communicate direction in various fields, including navigation, cartography, and...
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Relative Motion Analysis using Rotating Axes01:25

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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...
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Rocket Propulsion in Empty Space - I01:13

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The driving force for the motion of any vehicle is friction, but in the case of rocket propulsion in space, the friction force is not present. The motion of a rocket changes its velocity (and hence its momentum) by ejecting burned fuel gases, thus causing it to accelerate in the direction opposite to the velocity of the ejected fuel. In this situation, the mass and velocity of the rocket constantly change along with the total mass of ejected gases. Due to conservation of momentum, the...
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Kepler's Second Law of Planetary Motion01:29

Kepler's Second Law of Planetary Motion

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In the early 17th century, German astronomer and mathematician Johannes Kepler postulated three laws for the motion of planets in the solar system. His first law states that all planets orbit the Sun in an elliptical orbit, with the Sun at one of the ellipse's foci. Therefore, the distance of a planet from the Sun varies throughout its revolution around the Sun.
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Updated: Sep 19, 2025

3D Orbital Tracking in a Modified Two-photon Microscope: An Application to the Tracking of Intracellular Vesicles
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基于ADP的轨道跟踪控制器,用于在未知小行星周围飞行的深空探测器.

Zebin Chen, Yanwei Ding, Wenjian Tao

    IEEE transactions on neural networks and learning systems
    |June 19, 2025
    PubMed
    概括

    这项研究提出了一种新的自适应动态编程方法,用于深空探测器轨道跟踪在未知的小行星周围. 该方法确保稳定的控制,尽管不可预测的动态,通过模拟验证.

    科学领域:

    • 航空航天工程 航空航天工程
    • 控制理论 控制理论
    • 机器人技术 机器人技术 机器人技术

    背景情况:

    • 深空任务需要精确的轨道跟踪探测器靠近天体.
    • 未知的小行星动态对传统的控制系统构成重大挑战.
    • 现有的方法通常依赖于准确的模型,而这些模型在深空探索中是不可用的.

    研究的目的:

    • 开发一个强大的轨道跟踪控制策略,用于深空探测器周围的小行星与未知的动态.
    • 使用自适应动态编程设计基于模型的最佳控制器和无模型的次优控制器.
    • 通过数值模拟来确保非对称稳定性和验证拟议的控制方法.

    主要方法:

    • 建立一个相对运动轨道跟踪控制模型.
    • 基于模型的最佳控制器的设计,具有经过验证的非对称稳定性.
    • 适应式动态编程 (ADP) 算法的应用,基于对无模型控制器的策略代.
    • 在线数据收集用于构建和解决用于控制器参数识别的高阶线性方程.

    主要成果:

    • 一个基于模型的控制器,证明了闭环系统的非对称稳定性.
    • 一个使用ADP推导的无模型次优控制器,该控制器近似于基于模型的控制器.

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  • 通过数值模拟成功验证控制方法的有效性和性能.
  • 证明了在轨道跟踪中处理完全未知的动态的能力.
  • 结论:

    • 拟议的自适应动态编程方法为深空探测器在未知的动态下轨道跟踪提供了有效的解决方案.
    • 基于模型和无模型的控制策略的组合提供了稳定性和适应性.
    • 该方法被验证为未来需要精确轨迹控制的深空探索任务的可靠工具.