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

Claim 2:
3. The spacecraft thrusters control system according to claim 2, wherein
the constraint dimensionality is smaller than the variable dimensionality,
the variable vector is nonnegative,
the simultaneous formulas are simultaneous equations,
the dual constraints are inequality constraints equal in number to the variable dimensionality and represented by a transposed matrix of the constraint coefficient matrix,
the optimal solution calculation device includes an optimal active set computator to find an active set maximizing the determined inner product as the optimal active set, and
the matrix from which the optimal solution computator finds the inverse matrix is a matrix having an arrangement of a column vector included in the constraint coefficient matrix and corresponding to the formula identifiers of the optimal active set.