Motivation, Computation and Applications of Quasi-Periodic Orbits in Space Trajectory Design

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Motivation, Computation and Applications of Quasi-Periodic Orbits in Space Trajectory Design

김선우 0 8008
구분 기타
일정 2025-03-28(금) 14:00~16:00
세미나실 129동 104호
강연자 Daniel J. Sheeres (University of Colorado)
담당교수 Otto van Koert
기타

제목: Motivation, Computation and Applications of Quasi-Periodic Orbits in Space Trajectory Design

초록: The application of dynamical systems methods to the design of spacecraft trajectories has resulted in a robust and rich approach to developing transfers in multi-body problems. Perhaps the most elegant approach to these designs are the use of invariant orbits and their stable and unstable manifolds to effect transfers that can move across large distances in space. Most specific applications in this realm have focused on using simple invariant orbits such as periodic orbits and their manifolds to find candidate heteroclinic connections. However, the existence of higher-dimensional invariant orbits such as quasi-periodic orbits and their related manifolds has not been studied as closely, due to the difficulty in precisely computing these objects in general situations.

Recent research at the University of Colorado (CU) have implemented robust computational algorithms for precisely finding and continuing quasi-periodic orbits of dimension 2 and higher, along with their manifolds (Z. Olikara, PhD. Thesis, 2016). The use of these higher-dimensional orbits can have significant impacts on the design of heteroclinic transfers, along with many other applications. This arises due to the relatively high phase space co-dimensions of the stable and unstable manifolds of these orbits, making it is easier to find connections between different quasi-periodic tori of the same energy. Similarly, the ability to compute these higher-dimensional tori also enables the robust continuation of periodic orbits and tori in periodically perturbed problems, such as the elliptic-restricted 3-body problem or the problem of orbiting about an asteroid in a complex rotation state. There are also significant applications to orbit mechanics in complex environments and formation flight of satellites. This talk will describe our recent, current and future research on these problems. 

    정원 : 57석
    부속시설 : 칠판, 프로젝터, 강사추적 카메라,무선랜, 전자교탁(PC)
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