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ENHANCED GROUND BASED PRECISE ATTITUDE DETERMINATION METHOD OF IMAGING SATELLITE

机译:基于增强地面的卫星精确姿态确定方法

摘要

PURPOSE: An enhanced ground based precise posture determination method of a low-orbit imaging satellite is provided to accurately determine the posture of the satellite by dually using gyro measurement data and star tracker measurement data. CONSTITUTION: Gyro measurement data and star tracker measurement data are obtained in different intervals through a gyro sensor and a star tracker using a dual MIL-STD-1553 bus communication device (S100). The gyro measurement data and the star tracker measurement data are stored and transmitted to a ground station (S200). A posture quaternion estimated value is repeatedly predicted until the star tracker measurement data is received after calculating an angular speed by restoring the transmitted gyro measurement data again (S300). A modified value is calculated by using the posture quaternion estimated value and the star tracker measurement data, and an error posture quaternion is applied as a corrected value by using the modified value (S400). [Reference numerals] (S100) Measured data obtaining step; (S200) Measured data transmitting step; (S300) Angular speed calculating and predicting step; (S400) Correcting step
机译:目的:提供一种改进的低轨道成像卫星的基于地面的精确姿态确定方法,以通过同时使用陀螺仪测量数据和恒星跟踪器测量数据来精确确定卫星的姿态。组成:陀螺仪测量数据和恒星跟踪仪测量数据是使用双MIL-STD-1553总线通信设备通过陀螺仪传感器和恒星跟踪仪以不同的间隔获得的(S100)。陀螺仪测量数据和恒星跟踪仪测量数据被存储并发送到地面站(S200)。重复预测姿势四元数估计值,直到通过再次恢复发送的陀螺仪测量数据来计算角速度之后接收到星形跟踪器测量数据为止(S300)。通过使用姿势四元数估计值和星形跟踪器测量数据来计算修改值,并且通过使用修改后的值将错误姿势四元数用作校正值(S400)。 [附图标记](S100)测量数据获取步骤; (S200)实测数据发送步骤; (S300)角速度计算预测步骤; (S400)校正步骤

著录项

  • 公开/公告号KR101294623B1

    专利类型

  • 公开/公告日2013-08-08

    原文格式PDF

  • 申请/专利权人 KOREA AEROSPACE RESEARCH INSTITUTE;

    申请/专利号KR20120157528

  • 发明设计人 PARK KEUN JOO;LEE YUN KI;

    申请日2012-12-28

  • 分类号G05D1/08;G05D3;

  • 国家 KR

  • 入库时间 2022-08-21 16:24:43

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