Patent ID: 11958635
Assignee: MITSUBISHI ELECTRIC CORPORATION
Field: Transport (Mechanical engineering)
Classification: CPC B  G | IPC B  G

Claim 1:
2. The spacecraft thrusters control system according to claim 1, wherein
the dual solution candidate searcher determines the dual problem as a problem including dual constraints having formulas equal in number to the variable dimensionality,
the active sets are each expressed as formula identifiers indicating, among the formulas in the dual constraints, a combination of active formulas equal in number to a smaller one of the variable dimensionality and the constraint dimensionality,
the feasible dual solution candidate is a solution vector satisfying the formulas in the dual constraints indicated by the formula identifiers in the corresponding active set, and
the optimal solution calculation device includes an optimal solution computator to find an optimal solution to the variable vector based on a product of the constraint vector and an inverse matrix of a matrix found from the constraint coefficient matrix using information about the optimal active set.