Algorithms for guidance and digital attitude control of a maneuvering land-survey satellite

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We present algorithms for synthesis of the vector spline guidance laws and the digital attitude control laws for a land-survey satellite when it is fulfilling a sequence of the routes with a scanning optoelectronic observation and the rotational maneuvers with general boundary conditions.

Land-survey satellite, orientation, guidance, digital control

Короткий адрес: https://sciup.org/148204831

IDR: 148204831

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