Net capture orientation design method based on waste satellite attitude motion characteristics

The invention relates to a net capture orientation design method based on waste satellite attitude motion characteristics, and belongs to the technical field of aircraft net capture of waste satellites. The method comprises the following steps of: 1, acquiring historical attitude motion characterist...

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Bibliographic Details
Main Authors ZHANG QINGZHAN, CHEN JIZHENG, YUAN CHAO, HAO XIAOLONG, WANG CHUANZONG, YANG GUANGLIE, WANG HONGYU
Format Patent
LanguageChinese
English
Published 30.03.2021
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Summary:The invention relates to a net capture orientation design method based on waste satellite attitude motion characteristics, and belongs to the technical field of aircraft net capture of waste satellites. The method comprises the following steps of: 1, acquiring historical attitude motion characteristic parameters of a waste satellite, wherein the historical attitude motion characteristic parameterscomprise an attitude angular velocity omega, a maximum nutation angle theta max and a minimum nutation angle theta min; 2, setting an attitude stabilization angular velocity threshold omega0 and a net capture load adaptive angle threshold theta0; and 3, according to the attitude angular velocity omega, the maximum nutation angle theta max, the minimum nutation angle theta min, an attitude stableangular speed threshold omega 0 and a net capture load adaptive angle threshold theta 0, determining the net capture direction of the waste satellite; according to the waste satellite attitude motioncharacteristic parameters,
Bibliography:Application Number: CN202011480364