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Paulo Renato Silva, Ivanildo Silva Abreu, Paulo Almeida Forte, Henrique Mariano Costa do Amaral
Pág. 150 - 161
For proper attitude control of space-crafts conventional optimal Linear Quadratic (LQ) controllers are designed via trial-and-error selection of the weighting matrices. This time consuming method is inefficient and usually results in a high order complex...
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