О нагрузках на элементы конструкции Многоцелевого лабораторного модуля на автономном участке полета

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О нагрузках на элементы конструкцииМногоцелевого лабораторного модуля…
ISSN 0236-3933. Вестник МГТУ им. Н.Э. Баумана. Сер. Приборостроение. 2017. № 2 137
Abstract Keywords
This purpose of this work was to solve the task of estima-
ting multipurpose laboratory module construction
strength. Algorithms for calculating the loads on the solar
array drive assembly are integrated into a closed motion
simulation loop as part of the workstation of guidance,
navigation and control system algorithms developer. In
the modeling process on each computational cycle when
the actuators (whose function is performed by jet en-
gines) were working, we calculated the loads on solar
battery drives. As a part of the stand we built the format
for controlling the forces and moments acting on the
solar array drive assembly as a result of the work of gui-
dance, navigation and control system. Moreover, we
managed to implement the control of critical load level
excess
International Space Station, multi-
purpose laboratory module, Russian
segment, eigenfrequencies, loads on
construction, guidance, navigation
and control system
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