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Determination of the Attitude of the Skylark Rocket from a Conical Scanning Sun-Slit and Magnetometers

机译:从锥形扫描太阳裂缝和磁强计确定云雀火箭的姿态

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The Memorandum describes the determination of the attitude of the Skylark rocket, using a conical scanning sun-slit and an orthogonal array of magnetometers, at the time of a pulse from the sun-slit. There are two attitudes which satisfy the data. The correct solution must be chosen by appealing to other information e.g. continuity of the attitude motion. (Author)

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