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Alternative TitleDouble layer structure predictive control method for steady state optimization value used in aviation
邹涛; 郑洪宇; 张鑫; 李永民; 庞强; 王景扬; 郑东梁; 曹宇; 魏来星
Rights Holder中国科学院沈阳自动化研究所
Patent Agent沈阳科苑专利商标代理有限公司 21002
Other AbstractThe method involves generating (S1) objective functions and forming linear programming problems. An off-line data table is created (S2) by solving linear programming problems by offline. The steady-state optimization value of next time is obtained (S3) through offline lookup of offline data tables. The steady-state optimization value of the upper layer is passed (S4) to the dynamic control layer at the lower level, and is used as the setting value of the dynamic control layer, and is calculated by the dynamic control algorithm.
PCT Attributes
Application Date2015-10-30
Date Available2019-07-16
Application NumberCN201510725636.7
Open (Notice) NumberCN106647250A
Contribution Rank1
Document Type专利
Recommended Citation
GB/T 7714
邹涛,郑洪宇,张鑫,等. 基于离线优化/在线查表方式的双层结构预测控制方法[P]. 2017-05-10.
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