System and method for sensing attitude of a spacecraft with equilized star tracker errors along three orthogonal axes

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  机译： 沿三个正交轴的均等恒星跟踪器误差感测航天器姿态的系统和方法

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  机译： 自主校正恒星跟踪器电荷转移效率误差的航天器方法和系统

• 5. SPACECRAFT METHODS AND SYSTEMS FOR AUTONOMOUS CORRECTION OF STAR TRACKER CHARGE-TRANSFER-EFFICIENCY ERRORS [P] . 美国专利： US2002125375A1 . 2002-09-12

  机译： 自动校正星型跟踪器电荷转移效率误差的空间工艺方法和系统

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