首页> 外文会议>13th international technical meeting of the Satellite Division of the Institute of Navigation (ION GPS-2000) >Spacecraft Attitude Determination using a Combination of GPS Attitude Sensor and Star Sensor Measurements
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Spacecraft Attitude Determination using a Combination of GPS Attitude Sensor and Star Sensor Measurements

机译:结合GPS姿态传感器和恒星传感器测量结果确定航天器姿态

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The applications of GPS in space, such as orbit andrnattitude determination, offer several advantages, e.g.rncomplete navigation information on board, low weight,rnvolume and power consumption.rnGPS based attitude determination has many importantrnadvantages like the fast and reliable initial acquisition, thernresistance against spin rates and the fact, that at least twornsatellites for deterministic attitude determination arernalways visible during the mission. GPS could also be usedrnas a safe mode sensor. Therefore GPS based attituderndetermination seems very promising. But due to thernachievable accuracy, implied by the baseline length andrnthe signal noise, a GPS attitude sensor cannot be used forrnmissions where high accurate attitude measurements arernneeded and the baseline lengths are restricted.rnFor these missions, a star sensor will be the adequaternattitude sensor. Star sensors are high accurate, robust andrnhave well established algorithms. The disadvantagesrnusing star sensors are e.g. restricted field of view,rnoperation only at low angular rates, sensor performancerndegradation and sometimes problems with the starrnidentification.rnTaking all these individual advantages and disadvantagesrninto account, the combination of a GPS attitude sensorrnand a star sensor seems extremely promising, becausernsuch a sensor combination can be applied to a broad arearnof missions and their requirements of a high accuraternattitude.rnA study project has therefore been initiated atrnDLR/GSOC, which deals with the development of newrnalgorithms for the combination of a GPS attitude sensorrnand a star sensor and the investigation of the variousrnpossibilities to support each other and therefore improvernthe attitude solution and the range of applicability.rnPreliminary results presented in this paper are obtainedrnfrom an experiment on a turn table with a four antennarnGPS attitude sensor and a star sensor on top of it during arnground night experiment.
机译:GPS在空间中的应用(例如确定轨道和高度)具有许多优势,例如,机载完整的导航信息,重量轻,体积小和功耗低。基于GPS的姿态确定具有许多重要的优点,例如快速可靠的初始获取,防旋转能力率和事实,即在任务期间始终至少可见两个用于确定性姿态确定的卫星。 GPS也可以用作安全模式传感器。因此,基于GPS的姿态确定似乎很有希望。但是由于基线长度和信号噪声暗示着可以实现的精度,因此在需要高精度姿态测量且基线长度受到限制的GPS姿态传感器中,不能使用GPS姿态传感器。对于这些任务,星形传感器将是足够的姿态传感器。星型传感器是高精度,鲁棒性强的算法。使用星形传感器的缺点是例如受限的视野,仅在低角速率下运行,传感器性能下降以及有时出现恒星识别问题。考虑到所有这些优点和缺点,GPS姿态传感器和恒星传感器的组合似乎非常有前途,因为这样的传感器组合可以因此,在DLR / GSOC上启动了一项研究项目,该项目致力于开发GPS姿态传感器和星型传感器相结合的新算法,并研究各种可能的方法。相互支持,从而改善了姿态解决方案和适用范围。本文是从在转台上进行的实验获得的初步结果,该转台上有四个天线GPS姿态传感器和一个星型传感器,在arnground夜间实验中。

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