Abstract
In physics, an equilibrium point means the positions in body-fixed frame Oxyz where the gravity from the small body and the centrifugal force balance. For a real small body which has irregular overlook, the equilibrium points are usually isolated and of finite number. This chapter takes the equilibria as a start of surveying the system dynamic behaviours, not only because of its simplicity, but also that the equilibria may be a key to understand the global orbital behaviours. As shown by Eq. 3.1, an equilibrium point is also a critical point of the contour surfaces of the efficient potential V, which is correlated to the topological evolution of these surfaces (see Sect. 2.5 for the discussion on \(\kappa \)). In this chapter, we take a specific asteroid for example, and discuss the orbital motion within the neighbourhoods of equilibrium points using the polyhedral gravity model. Section 3.2 calculates the equilibrium points of the target body, and presents the geometry and topology of the contour surfaces of efficient potential V. Sections 3.3 and 3.4 use the linearized theory to determine the stability and type of an equilibrium point, and reveal the orbital motion on local invariant manifolds. Based on the analysis of local manifolds, Sect. 3.5 further discusses the general orbital patterns in the neighbourhoods of the equilibrium points.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsReferences
Ostro SJ, Hudson RS, Nolan MC et al (2000) Radar observations of asteroid 216 Kleopatra. Science 288:836–839
Descamps P, Marchis F, Berthier J et al (2011) Triplicity and physical characteristics of asteroid (216) Kleopatra. Icarus 211:1022–1033
Szebehely V (1967) Theory of orbits: the restricted problem of three bodies. Academic Press Inc., New York
Liu Y, Chen L (2001) Nonlinear vibration. Higher Education Press, Beijing
Hu W, Scheeres DJ (2004) Numerical determination of stability regions for orbital motion in uniformly rotating second degree and order gravity fields. Planetary and Space Science 52:685–692
Perko L (1991) Differential equation and dynamical system. Springer, New York
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2016 Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
Yu, Y. (2016). Stability of Equilibrium Points and Behaviour of Nearby Trajectories. In: Orbital Dynamics in the Gravitational Field of Small Bodies. Springer Theses. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-52693-4_3
Download citation
DOI: https://doi.org/10.1007/978-3-662-52693-4_3
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-662-52691-0
Online ISBN: 978-3-662-52693-4
eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)