首页> 外文会议>ESA Symposium on European Rocket and Balloon Programmes and Related Research >GRANASAT MULTI-SENSOR ATTITUDE DETERMINATION SYSTEM TESTED IN BEXUS19 STRATOSPHERIC BALLOON
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GRANASAT MULTI-SENSOR ATTITUDE DETERMINATION SYSTEM TESTED IN BEXUS19 STRATOSPHERIC BALLOON

机译:在BEXUS19球面气球上测试的GRANASAT多传感器姿态测定系统

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GranaSAT designed and built a low-cost attitude determination system, a fundamental system for any spacecraft, based on a star and horizon sensor, acceleration and Earth's magnetic field measurements. The same Charge Coupled Device was used for both the star sensor and the horizon sensor. For the star sensor the Lost in Space functionality was designed, the identification algorithm used is a variation of the Matching Group algorithm proposed by Van Benzooijen; for the horizon sensor a simple detection algorithm is proposed, with the circle fitting method based on Umbach and Jones work, and for the magnetometer and accelerometer sensors the attitude was estimated by a two vector matching procedure based on Wahba solution.
机译:GranaSAT设计并构建了一种低成本的姿态确定系统,该系统是基于星空和地平线传感器,加速度和地球磁场测量结果的所有航天器的基本系统。星形传感器和水平传感器都使用了相同的电荷耦合器件。对于星形传感器,设计了“迷失太空”功能,所用的识别算法是范本苏仁提出的匹配组算法的一种变体。针对水平传感器,提出了一种简单的检测算法,采用基于Umbach和Jones的圆拟合方法,对于磁力计和加速度计传感器,通过基于Wahba解的两个矢量匹配程序来估计姿态。

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