FIELD: astronautics.SUBSTANCE: invention relates to spacecraft orientation control, carried out in the solar-terrestrial coordinate system. Method includes orienting the first axis of spacecraft towards the Earth by turning around the second and third axes of the spacecraft using electromechanical actuators. In the absence of Earth's shadow, control actions around the second axis of the spacecraft are generated based on information from the instrument for orientation towards the Earth, and relative to the third axis of the spacecraft – based on information from the instrument for orientation towards the Sun.EFFECT: technical result is reduced error of orientation of spacecraft towards the Earth.1 cl, 3 dwg
СПОСОБ ОРИЕНТАЦИИ КОСМИЧЕСКОГО АППАРАТА В СОЛНЕЧНО-ЗЕМНОЙ СИСТЕМЕ КООРДИНАТ
28.09.2017
Patent
Elektronische Ressource
Russisch
Europäisches Patentamt | 2018
КОМБИНИРОВАННАЯ ГРАВИТАЦИОННАЯ СИСТЕМА ОРИЕНТАЦИИ МАЛОГО КОСМИЧЕСКОГО АППАРАТА
Europäisches Patentamt | 2017
Europäisches Patentamt | 2018