Abstract
Petri Nets is very interesting tool for studying and simulating different behaviors of automatic systems. It can be used in different applications based on the appropriate class of Petri Nets (e.g. colored, timed, or higher order Petri Nets). In this paper, a novel Petri Net approach called Orbital Petri Nets (OPN) is proposed for studying the dynamic behaviour of orbital auto-systems such as satellites motion. This initial study introduced a theoretical analysis of OPN with highlighting the problem of space debris collision as a case study. By this novel approach of Petri Nets, new smart algorithms can be implemented and simulated for handling several space problems, such as satellites’ maneuvers or debris disposal.
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