摘要: |
星载陀螺组合的零偏稳定性将直接影响姿轨控分系统对姿态变化的测量精度。针对影响半球谐振陀螺组合输出零偏稳定性的因素进行了分析,研究了温度影响输出变化的机理,并提出了相应的解决措施。工程实践表明,这些措施以较低的成本有效地提升了半球谐振陀螺组合的零偏稳定性。 |
关键词: 半球谐振陀螺组合 零偏稳定性 误差分析 温度控制 |
DOI: |
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Research on the Technology of Improving the Zero-bias Stability of theHemispherical Resonator Gyroscope Unit |
QI Yi-nan,ZHAO Hui,ZHAO Wan-liang,ZHANG Qiang |
(Shanghai Jiao Tong University;Shanghai Aerospase Control Technology Institute) |
Abstract: |
The stability of the satellite-bone gyroscope combination will directly affect the measurement accuracy of attitude variation tested by an attitude and orbit control system.The factors of output zero-offset stability which affect the hemispherical resonator gyroscope unit are analyzed in this paper,and the mechanism of temperatures impact on output variation is studied,with the relevant solutions proposed.The engineering practice shows that these measures improve effectively the zero-bias stability of the hemispherical resonator gyroscope unit at lower costs. |
Key words: Hemispherical resonator gyroscope unit Zero-bias stability Error analysis Temperature control |