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8
Issue
vol 63 / August, 2020
Article

DOI 10.17586/0021-3454-2020-63-6-522-527

UDC 629.7.01

MODELLING ROTATIONS OF SOLAR CELLS ON A SPACE VEHICLE. ADEQUACY CHECK

Овчаренко В. А.
АО "Конструкторское бюро "Арсенал" им. М.В. Фрунзе"; инженер 1 категории


Пилецкий А. В.
ОАО "Машиностроительный завод "Арсенал"; инженер 1 категории


Бурлуцкий С. Г.
Санкт-Петербургский государственный университет аэрокосмического приборостроения, кафедра эксплуатации и управления аэрокосмическими системами;


Abstract. A mathematical model describing the influence of the main ballistic parameters of an artificial Earth satellite flight on orientation of its solar panels is considered. The model adequacy is checked using a presented test.
Keywords: flight parameters, solar panels, orientation, adequacy

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