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大型充液卫星在轨模式识别
引用本文:孙宝祥,邹广瑞,吕振铎.大型充液卫星在轨模式识别[J].航天控制,2000(4).
作者姓名:孙宝祥  邹广瑞  吕振铎
作者单位:北京控制工程研究所!北京100080
摘    要:提出了大型充液卫星在轨模式识别的方法 ,通过大型充液卫星在轨飞行试验确定液体晃动阻尼 ,为控制系统设计中确定晃动阻尼提供最可靠的依据

关 键 词:卫星  模式识别  姿态控制  推进剂  晃动阻尼

On-Board Pattern Recognition for Large Satellites with Tanks Filled with Propellants
Sun Baoxiang\ Zou Guangrui\ Lu Zhenduo Beijing Institute of Control Engineering,Beijing.On-Board Pattern Recognition for Large Satellites with Tanks Filled with Propellants[J].Aerospace Control,2000(4).
Authors:Sun Baoxiang\ Zou Guangrui\ Lu Zhenduo Beijing Institute of Control Engineering  Beijing
Institution:Sun Baoxiang\ Zou Guangrui\ Lu Zhenduo Beijing Institute of Control Engineering,Beijing 100080
Abstract:In this paper an on-board pattern recognition method for large satellites with tanks filled with propellants is presented to determinate the damp ratios of propellant sloshing by means of flight tests, and to provide reliable information for the attitude control system design.
Keywords:Satellite\ Pattern recognition\ Attitude control\ Propellant\ Sloshing\ dampip
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