Satellite Conceptual Design Multi-Objective Optimization Using Co Framework

A. Jafarsalehi؛ M. Mirshams؛ R. Emami

دوره 7، شماره 1 ، فروردین 1393

  This paper focuses upon the development of an efficient method for conceptual design optimization of a satellite. There are many option for a satellite subsystems that could be choice, as acceptable solution to implement of a space system mission. Every option should be assessment based on the different criteria such as cost, mass, reliability and technology contraint (complexity). In this research, mass and technology constraints, which have a direct impact on the satellite life cycle cost, are considerd as system level objective function to obtain the system optimal solution during the coceptual ...  بیشتر