Author/Authors :
Aram, A. sharif university of technology - School of Mechanical Engineering, تهران, ايران , Zohoor, H. sharif university of technology - Center of Excellence in Design, Robotics and Automation, تهران, ايران , Zohoor, H. Academy of Sciences of IR Iran, ايران , Sohrabpour, S. sharif university of technology - Center of Excellence in Design, Robotics and Automation, تهران, ايران , Sohrabpour, S. Academy of Sciences of I. R. of Iran, ايران
Abstract :
Periodic orbits have been studied more extensively by space mission designers in recent years. These orbits are usually described as planar in three-body-problems. In this article, in addition to introducing a new orbit that turns around a secondary mass, applications in Moon-based, Earth-based, and interplanetary missions are also described. Floquet exponents as chaos indicators and normal potential levels for orbits are also calculated. The advantages of their use as space station orbits are studied at the end of the article.
Keywords :
Restricted three body problem , Periodic orbits , Floquet exponent , Floquet theory , Space station.
