It can be seen that under this special condition, the discrete- time state equation is still conditionally linear so that there is no need to use multistep propagation any more. Therefore, MUKF will ...
A spacecraft attitude kinematics model, attitude measurement model, and filter algorithm are three important parts in spacecraft attitude determination, and a high-precision filtering algorithm is the ...
A spacecraft attitude kinematics model, attitude measurement model, and filter algorithm are three important parts in spacecraft attitude determination, and a high-precision filtering algorithm is the ...
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