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Linear Approximation in Time Domain01:21

Linear Approximation in Time Domain

379
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,...
379
Feedback control systems01:26

Feedback control systems

735
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...
735
Time-Domain Interpretation of PD Control01:07

Time-Domain Interpretation of PD Control

415
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...
415
Controller Configurations01:22

Controller Configurations

399
Controller configurations are crucial in a car's cruise control system because they manage speed over time to maintain a consistent pace regardless of road conditions, thereby meeting design goals. In traditional control systems, fixed-configuration design involves predetermined controller placement. System performance modifications are known as compensation.
Control-system compensation involves various configurations, most commonly series or cascade compensation, in which the controller...
399
Linear Momentum in Control Volume01:13

Linear Momentum in Control Volume

1.3K
Newton's second law is applied to obtain the linear momentum in a control volume in a fluid system. According to this law, the rate of change of linear momentum is equal to the sum of external forces acting on the system. When a control volume matches the fluid system at a specific moment, the forces acting on both are identical. Reynolds transport theorem helps explain this by breaking down the system's linear momentum into two components: the rate of change of linear momentum within...
1.3K
Multi-input and Multi-variable systems01:22

Multi-input and Multi-variable systems

431
Cruise control systems in cars are designed as multi-input systems to maintain a driver's desired speed while compensating for external disturbances such as changes in terrain. The block diagram for a cruise control system typically includes two main inputs: the desired speed set by the driver and any external disturbances, such as the incline of the road. By adjusting the engine throttle, the system maintains the vehicle's speed as close to the desired value as possible.
In the absence of...
431

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相关实验视频

Updated: Feb 20, 2026

Gain-compensation Methodology for a Sinusoidal Scan of a Galvanometer Mirror in Proportional-Integral-Differential Control Using Pre-emphasis Techniques
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抗解时间变化的滑动模式控制与任意收时间对刚性航天器的时间.

Yu-Tian Xu, Youmin Gong, Ai-Guo Wu

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    概括
    此摘要是机器生成的。

    这项研究为刚性航天器提供了一种新的姿态机动控制,使得任意的收时间成为可能. 新的控制法确保了稳定性,并避免了放松现象.

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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

    背景情况:

    • 太空飞船的态度控制对于任务的成功至关重要.
    • 实现准确和快速的态度机动,保证稳定是一个持续的挑战.

    研究的目的:

    • 为刚性航天器开发一种新的态度机动控制法.
    • 为了实现任意的趋同时间来稳定态度.
    • 为了防止航天器态度控制中的不良解现象.

    主要方法:

    • 设计一个时间变化的滑动模式函数,使用一块指数函数.
    • 基于设计的滑动模式功能的态度控制规律的开发.
    • 对系统稳定性和收性质的分析.

    主要成果:

    • 拟议的控制法确保闭环态度系统状态从最初的时间保持在滑动模式表面上.
    • 向原点的态度收是在任意预设的时间内实现的.
    • 建议的控制策略有效地避免了解现象.

    结论:

    • 开发的态度控制法提供了对航天器机动的精确和灵活的控制.
    • 该方法提供了一个可靠的解决方案,可以实现所需的融合时间,同时确保稳定性.
    • 这种方法提高了航天器态度控制系统的可靠性和性能.