Autonomous guidance and attitude control of a spacecraft in tracking mode

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A new method of autonomous guidance and digital control of the spacecraft orientation in the mode of tracking changes in the vector of modified Rodrigue parameters is presented. Numerical results on the efficiency of the developed algorithms used for information satellites and space robots are represented.

Spacecraft, autonomous angular guidance, orientation digital control

Короткий адрес: https://sciup.org/148314203

IDR: 148314203

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