Large space structure integrated structural and control optimization, using analytical sensitivity analysis

被引:3
作者
Fonseca, IM
Bainum, PM
机构
[1] Natl Inst Space Res, Space Mech & Control Div, BR-12201970 Sao Jose Dos Campos, Brazil
[2] Howard Univ, Dept Mech Engn, Washington, DC 20059 USA
关键词
D O I
10.2514/2.4805
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The analytical sensitivity analysis procedure to implement the integrated structural and control optimization of a large, low-Earth-orbit space structure is dealt with. The objective is to show that significant computation time can be saved when the analytical procedure is used instead of numerical calculation of the sensitivity. Despite that the numerical approach is attractive because it does not require the hard algebraic task to develop the sensitivity derivative expressions, the approach is often responsible for the major computational cost of an optimization process. The analytical approach represents an attractive option when the computational effort becomes prohibitive under cost considerations.
引用
收藏
页码:978 / 982
页数:5
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