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基于Rodrigues參數交互模型航天器相對位姿測量技術(shù)
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河南工業(yè)職業(yè)技術(shù)學(xué)院

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TN925

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Relative pose measurement technology of spacecraft based on Rodrigues parameter interaction model
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    摘要:

    針對傳統測量技術(shù)測量航天器相對位姿準確度較低的問(wèn)題,引用Rodrigues參數交互模型研究了一種新的航天器相對位姿測量技術(shù)。利用Rodrigues參數建立航天器位姿采集模型,通過(guò)原向量、旋轉軸、原向量和旋轉軸的交叉積等向量作為標架,獲得航天器旋轉以后得向量組,利用四元數定理來(lái)減少計算航天器旋轉向量的計算量,在觀(guān)察三維空間內的坐標系間的向量變化曲線(xiàn)規律后,測量出交互模型的航天器相對位姿,得出基于羅德里格旋轉參數交互模型結構圖,確定羅德里格旋轉參數模型與航天器的距離H和地面接收到的航天器相位位姿的誤差。通過(guò)Harris角點(diǎn)檢測方法計算航天器模擬圖像的每個(gè)像素和灰度,通過(guò)像素和灰度信息進(jìn)行條件隨機場(chǎng)計算,分析航天器相對位姿特征,在多次尋找三維坐標系中查找相似的最近臨近點(diǎn)和次臨近點(diǎn)后,合理匹配,確定航天器相對位姿。實(shí)驗結果表明,基于Rodrigues參數交互模型航天器相對位姿測量技術(shù)測量的精準度比傳統技術(shù)高出25.88%,實(shí)用性更強。

    Abstract:

    Traditional measurement techniques have low accuracy in measuring the relative pose of spacecraft. Aiming at the above problems, a new spacecraft relative position and attitude measurement technology was studied using the Rodrigues parameter interaction model. Rodrigues parameters are used to establish the spacecraft pose acquisition model. The original vector, the rotation axis, the cross product of the original vector and the rotation axis are used as frames to obtain the vector group obtained after the rotation of the spacecraft. The quaternion theorem is used to reduce the calculation of aerospace The calculation amount of the rotation vector of the spacecraft, after observing the law of the vector change curve between the coordinate systems in the three-dimensional space, the relative pose of the spacecraft of the interaction model is measured, and the structure diagram of the interaction model based on Rodrigue"s rotation parameters is obtained to determine Rodrigues. The distance H of the lattice rotation parameter model from the spacecraft and the phase and pose errors of the spacecraft received on the ground. Calculate each pixel and grayscale of the spacecraft simulation image by Harris corner detection method, perform conditional random field calculation based on the pixel and grayscale information, analyze the relative pose characteristics of the spacecraft, and find similar ones in the three-dimensional coordinate system for multiple searches After the nearest point and the second point are reasonably matched, the relative position of the spacecraft is determined. The experimental results show that the accuracy of spacecraft relative pose measurement technology based on Rodrigues parameter interaction model is 25.88% higher than that of traditional technology, and it is more practical.

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田九玲,楊永菊.基于Rodrigues參數交互模型航天器相對位姿測量技術(shù)計算機測量與控制[J].,2020,28(9):19-22.

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  • 收稿日期:2020-01-21
  • 最后修改日期:2020-03-06
  • 錄用日期:2020-03-06
  • 在線(xiàn)發(fā)布日期: 2020-09-16
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