| 检测质量对硅微机械框架振动陀螺影响的研究 |
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| 引用本文： | 阮爱武,郭秀中. 检测质量对硅微机械框架振动陀螺影响的研究[J]. 航空学报, 1997, 18(4): 489-492 |
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| 作者姓名： | 阮爱武 郭秀中 |
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| 作者单位： | 西北工业大学自动控制系(阮爱武)，南京航空航天大学３０４教研室(郭秀中) |
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| 摘 要： | 根据陀螺的动力学方程，从陀螺设计中的重要参数——内、外框架组件的等惯量约束条件和振动灵敏度等角度，探讨了检测质量对陀螺性能的影响，为微机械框架振动陀螺的设计提供了理论依据。
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| 关 键 词： | 微机械框架振动陀螺 检测质量 灵敏度 等惯量约束条件 |
| 收稿时间： | 1996-07-19; |
STUDY ON THE IMPACT OF PROOF MASS ON SILICON MICROMECHANICAL GIMBAL VIBRATING GYROSCOPE |
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| Ruan Aiwu. STUDY ON THE IMPACT OF PROOF MASS ON SILICON MICROMECHANICAL GIMBAL VIBRATING GYROSCOPE[J]. Acta Aeronautica et Astronautica Sinica, 1997, 18(4): 489-492 |
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| Authors: | Ruan Aiwu |
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| Affiliation: | 1. Automatic Control Department, Northwestern Polytechnical University, Xi′an, 7100722. Faculty 304, Nanjing University of Aeronautics &; Astronautics , Nanjing, 210016 |
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| Abstract: | The impact proof mass on the gyros performance is discussed on the basis of microgyro dynamic equation and several important parameters in the design of micromechanical vibrating gyros, including equivalent moment of inertia constraint conditions in the inner and outer gimbals, sensitivity, etc . This study will lay foundation for the gyros design in the near future. |
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| Keywords: | micromechanical gimbal vibrating gyroscope proof mass sensitivity equivalent moment of inertia constraint conditions |
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