单词 | flexible spacecraft | ||||
释义 | flexible spacecraft
例句释义: 挠性航天器,柔性航天器 1. This article presents a dynamic model for a large flexible spacecraft with its end mass undergoing a large angle, high speed maneuvering. 建立带附加质量大型挠性航天器大角度快速机动时的动力学模型。 hkxb.buaa.edu.cn 2. Researches on the dynamic and control for the flexible spacecraft usually use the modal of the flexible appendages. 研究柔性航天器的动力学与控制问题时,通常需要利用柔性附件的模态信息。 zgkj.cast.cn 3. The relation among parameters is derived and the stability of single axis flexible spacecraft attitude control system is studied. 推导系统参数间的关系式,分析挠性空间飞行器主轴姿态控制系统稳定性问题。 www.ilib.cn 4. The dynamic equations of flexible spacecraft are derived by introducing a moving coordinate frame. 首先建立了采用任意浮动参考系时的柔性航天器动力学方程; zgkj.cast.cn 5. Finally, it is considered that the stability of flexible spacecraft with liquid-filled multi-body system. 最后,讨论了多体系统充液挠性空间飞行器的稳定性问题。 www.magsci.org 6. The problem of robust attitude control for three-axial-stabilized flexible spacecraft is considered. 研究三轴稳定的挠性航天器姿态的鲁棒控制问题。 www.acabice.cn:8080 7. Active vibration suppression in flexible spacecraft with mismatched uncertainty via variable structure control 挠性航天器姿态机动的变结构主动振动抑制 www.ilib.cn 8. Vibration reduction of flexible spacecraft integrating CSVS with distributed piezoelectric actuators during attitude maneuver 分力合成和智能材料相结合的振动控制方法 www.ilib.cn 9. Modal Parameter Identification for Flexible Spacecraft Using Output-only Subspace Algorithm 仅利用输出信号的挠性航天器模态参数子空间在轨辨识算法 www.ilib.com.cn 10. Building the Dynamics Model and Simulating Circumstances for the Control of a Kind of Flexible Spacecraft 建立一类挠性航天器的动力学模型及面向控制的仿真环境 www.ilib.cn 1. Dynamic Modeling for Flexible Spacecraft Appendages with Nonlinear Deformation 考虑非线性变形的航天器柔性附件建模方法 www.ilib.cn 2. Variable Structure Control for Large Angle Maneuvering of Flexible Spacecraft with Bounded Controller 控制受限的挠性航天器大角度机动变结构控制 service.ilib.cn 3. Vibration Suppression of Time-Fuel Optimal Attitude Maneuver Control for Flexible Spacecraft 挠性飞行器时间燃料优化姿态机动控制的振动抑制 www.ilib.cn 4. Sliding mode with reference input-shaping control design for flexible spacecraft slewing maneuvers 挠性航天器旋转机动的输入成形变结构控制 www.ilib.cn 5. Adaptive Control Scheme and Experiment for Vibration Suppression of Flexible Spacecraft 挠性航天器振动抑制的自适应方法及实验研究 www.ilib.cn 6. Application of Fuzzy Variable Structure Control in the Attitude Maneuvering of Flexible Spacecraft 模糊变结构控制在挠性航天器姿态机动中的应用 www.ilib.cn 7. Sliding Mode Variable Structure Control for Large Angle Maneuvering of Flexible Spacecraft 挠性航天器大角度机动的滑模变结构控制 www.ilib.cn 8. Intelligent Control Research for High Precision Attitude of Flexible Spacecraft 挠性航天器高精度智能控制方案研究 www.ilib.cn 9. Variable Structure Control for Flexible Spacecraft with Input Nonlinearities During Attitude Maneuver 带有输入非线性的挠性航天器姿态机动变结构控制 ilib.cn 10. Active vibration control of flexible spacecraft during attitude maneuver 挠性航天器姿态机动的主动振动控制 ilib.cn 1. Variable Structure Control for Large Angle Maneuvering of Flexible Spacecraft 挠性航天器大角度机动的变结构控制 service.ilib.cn 2. Vibration Reduction of Attitude Control for Flexible Spacecraft 挠性飞行器姿态机动的振动抑制 www.ilib.cn 3. Flexible Spacecraft Attitude Control System Design Using Wheels 挠性飞行器飞轮姿态控制系统设计 ilib.cn 4. Angular momentum feedback control for flexible spacecraft 挠性卫星姿态的角动量反馈控制 www.ilib.cn 5. Modeling and dynamics analysis of liquid-filled flexible spacecraft 充液挠性航天器的建模与动力学分析 www.ilib.cn 6. Attitude dynamics model and control of liquid filled flexible spacecraft 挠性充液卫星姿态动力学建模研究 www.ilib.cn 7. Active Vibration Suppression of Flexible Spacecraft Based on Dynamic Output Feedback 基于动态输出反馈的挠性航天器主动振动抑制 scholar.ilib.cn |
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