Optimization approach to the aircraft weight and balance problem with the centre of gravity envelope constraints-Reference-Cited by-同舟云学术

Optimization approach to the aircraft weight and balance problem with the centre of gravity envelope constraints

Author:

Zhao Xiangling¹²,Yuan Yuan³,Dong Yun⁴^ORCID,Zhao Ren¹

Affiliation:

1. Key Laboratory of Data Analytics and Optimization for Smart Industry (Northeastern University) Ministry of Education Shenyang China

2. Department of Flight Operation College of Air Traffic Management Civil Aviation University of China Tianjin China

3. College of Economics and Management Shenyang Aerospace University Shenyang China

4. Liaoning Engineering Laboratory of Operations Analytics and Optimization for Smart Industry Northeastern University Shenyang China

Funder

National Natural Science Foundation of China

China Scholarship Council

Fundamental Research Funds for the Central Universities

Publisher

Institution of Engineering and Technology (IET)

Subject

Law,Mechanical Engineering,General Environmental Science,Transportation

Link

Reference44 articles.

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