design of layout optimization of component satellite by considering constraints of attitude determination and control system and electromagnetic compatibility using genetic algorithm

Considering the importance of the proper arrangement of components and subsystems in space systems in order to satisfy the control, thermal and telecommunication system requirements, this article deals with the optimal placement design of a sample satellite. Compliance with condition control constraints, which is one of the basic system requirements of the satellite, is primarily defined as constraint. Other requirements of satellite subsystems, including the non-overlapping condition, are taken into account according to importance and priority. After determining the appropriate optimization method, the objective function and the constraints of the problem, the optimization algorithm is presented and the optimal answers are extracted. Due to the importance of controlling the issue of electromagnetic compatibility and preventing destructive damage caused by it, the proper wiring design is done on the optimal designs in compliance with the defined requirements.