Driving control protection method for solar wing of space station

The invention discloses a space station solar wing driving control protection method. The method comprises software protection, hardware protection and transmission chain protection. Software protection is topmost layer protection, hardware protection is bottommost layer protection, transmission cha...

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Bibliographic Details
Main Authors QIU HAIHUI, FU PEIHUA, CEN QIFENG, CHANG XINGANG, DING CHENGHUA, ZHANG YONGJIE
Format Patent
LanguageChinese
English
Published 18.04.2023
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Summary:The invention discloses a space station solar wing driving control protection method. The method comprises software protection, hardware protection and transmission chain protection. Software protection is topmost layer protection, hardware protection is bottommost layer protection, transmission chain protection is middle layer protection, and the three layers of protection are organically combined. The software protection comprises automatic stalling protection after communication abnormity, solar wing maximum acceleration protection and friction resistance increase grading protection; the hardware protection comprises motor overcurrent protection, brake overcurrent protection and clutch overcurrent protection; transmission chain protection is action constraint protection among a motor, a brake, a clutch, a driving locking mechanism and a switching locking mechanism which are designed for protecting a transmission device of a solar wing of a space station. Aiming at the specific structural form and load char
Bibliography:Application Number: CN202211679402