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相关概念视频

Impact: Problem Solving01:26

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In an experiment conducted during a Mars mission, a rover propels a projectile with an initial velocity, and the projectile rebounds after colliding with the Martian surface. To ascertain the maximum height attained by the projectile after this collision, the known restitution coefficient and acceleration due to gravity are employed.
By designating the launch point as the origin and utilizing kinematic equations, the vertical component of the projectile's velocity at the point of impact is...
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A rocket's velocity in the presence of a gravitational field is decreased by the amount of force exerted by Earth's gravitational field, which opposes the motion of the rocket. If we consider thrust, that is, the force exerted on a rocket by the exhaust gases, then a rocket's thrust is greater in outer space than in the atmosphere or on a launch pad. In fact, gases are easier to expel in a vacuum.
A rocket's acceleration depends on three major factors, consistent with the...
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Orthogonal Trajectories01:26

Orthogonal Trajectories

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Orthogonal trajectories describe the geometric relationship between two families of curves that intersect each other at right angles. One illustrative case involves a family of parabolas that open sideways along the x-axis. These curves share a common shape but differ by a scaling parameter, resulting in a set of curves that all pass through the origin and widen at different rates.Determining Orthogonal TrajectoriesTo identify the orthogonal trajectories for these parabolas, the first step...
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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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Rockets range in size from small fireworks that ordinary people use to the enormous Saturn V that once propelled massive payloads toward the Moon. The propulsion of all rockets, jet engines, deflating balloons, and even squids and octopuses are explained by the same physical principle: Newton's third law of motion. The matter is forcefully ejected from a system, producing an equal and opposite reaction on what remains.
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Avoidance learning and learned helplessness are critical concepts in understanding behavioral responses to negative stimuli.
Avoidance learning occurs when an organism learns that a specific behavior can prevent an unpleasant outcome. For example, a student who receives a bad grade may start studying harder to avoid future poor grades. This behavior persists even when the negative outcome is no longer present. Avoidance learning is powerful because it maintains behavior in the absence of the...
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相关实验视频

Updated: Jan 17, 2026

Mimicking a Space Mission to Mars Using Hindlimb Unloading and Partial Weight Bearing in Rats
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强大的低推力轨迹设计用于行星间航天飞行:一种自适应的潜伏增强学习方法.

Han Gao, Yanghui Lin, Zhongqi Sun

    IEEE transactions on cybernetics
    |January 14, 2026
    PubMed
    概括

    这项研究引入了一种新的自适应潜伏强化学习 (RL) 方法,用于强大的航天器轨迹设计. 它通过使用学习的潜在变量进行控制,有效地处理不确定性,提高任务性能.

    科学领域:

    • 航空航天工程 航空航天工程
    • 人工智能的人工智能
    • 控制系统 控制系统

    背景情况:

    • 由于状态和观测不确定性,航天器轨迹设计面临着挑战.
    • 现有的方法很难减轻这些不确定性对控制性能的影响.

    研究的目的:

    • 在不确定性下为低推力航天器开发强大的轨迹设计方法.
    • 为了减轻不确定性对控制性能的不利影响,使用一种新的RL方法.

    主要方法:

    • 提出了一个基于顺序隐藏变量模型 (SLVM) 的自适应性隐藏强化学习 (RL) 方案.
    • 一个随机隐性近接政策优化 (SLPPO) 方案将SLVM表示学习与PPO集成.
    • 改进的密集奖励塑造机制提高了训练效率.

    主要成果:

    • 在SLPPO计划中,控制策略来自学习的随机潜变量,优于使用原始观测的方法.
    • 两个交会任务的数值模拟表明了拟议方法的有效性.
    • 该方法成功地减轻了不确定性对航天器控制的不利影响.

    结论:

    • 拟议的自适应潜伏RL方案为不确定性下的航天器轨迹设计提供了强大的解决方案.

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  • 这种方法提高了复杂太空任务中的控制性能和训练效率.
  • 该方法已被验证用于实际应用,如约会任务.