APPLICATION OF A NUMERICAL METHOD FOR SOLVING EQUATIONS OF ORBITAL METERING AND CONNECTIONS INSPACE

It is felt necessary to provide new and e ective methods due to the importanceand need for orbital meetings and connections in space with respect to the launch ofspace stations and projects. This article focuses on exploring orbital meetings andconnections in space that are required in many space projects. Speci ed using rel-ative motion equations for circular and elliptic circuits of motion equations of twospacecraft relative to each other and the relationship between the spacecraft movesrelative to each other will be examined using the Clovis-Wiltshire relationship. Giventhe complexity of the equations, it is not possible to solve the problem using analyt-ical methods therefore, we try to solve using numerical methods. An application ofevolutionary algorithms to solve complex problems in the dynamics of moving objectshas been seen on several issues. There are complex and nonlinear equations in thistype of problem. The use of these methods in solving engineering problems

کلیدواژه ها:

Orbital meetings ، Evolutionary Algorithm ، Genetic Algorithm