Design optimization problems

in space science

Objective function evaluation softwares of multiobjective design optimization problems in space science are distributed so that they can be used as a test function for research and development of design optimization methods for real-world applications.

1. Conceptual design optimization of a hybrid rocket
to be comming !

2. Trajectory design optimization for the next Japanese solar observation mission SOLAR-C
Reference (in Japanese) Reference (in English) software package
the original version is uploaded (2010.12.20)

Akira Oyama
Department of Space Transportation Engineering
Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency
http://flab.eng.isas.jaxa.jp/member/oyama/index2e.html
oyama2flab.isas.jaxa.jp