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[[Image:Lissajous_orbit_l2.jpg|thumb|300px|Lissajous orbit around L2]]
In [[orbital mechanics]], a '''Lissajous orbit''' is a quasi-periodic orbital trajectory that an object can follow around a collinear [[libration point]] ([[Lagrangian point]]) of a three-body system without requiring any propulsion. '''Lyapunov orbits''' around a libration point are curved paths that lie ''entirely'' in the plane of the two primary bodies. In contrast, Lissajous orbits include components in this plane and perpendicular to it, and follow a [[Lissajous curve]]. [[Halo orbit]]s also include components perpendicular to the plane, but they are periodic, while Lissajous orbits are not.
In [[orbital mechanics]], a '''Lissajous orbit''' is a quasi-periodic orbital trajectory that an object can follow around a collinear [[libration point]] ([[Lagrangian point]]) of a three-body system without requiring any propulsion. '''Lyapunov orbits''' around a libration point are curved paths that lie ''entirely'' in the plane of the two primary bodies. In contrast, Lissajous orbits include components in this plane and perpendicular to it, and follow a [[Lissajous curve]]. [[Halo orbit]]s also include components perpendicular to the plane, but they are periodic, while Lissajous orbits are not.



Revision as of 23:53, 14 May 2009

Lissajous orbit around L2

In orbital mechanics, a Lissajous orbit is a quasi-periodic orbital trajectory that an object can follow around a collinear libration point (Lagrangian point) of a three-body system without requiring any propulsion. Lyapunov orbits around a libration point are curved paths that lie entirely in the plane of the two primary bodies. In contrast, Lissajous orbits include components in this plane and perpendicular to it, and follow a Lissajous curve. Halo orbits also include components perpendicular to the plane, but they are periodic, while Lissajous orbits are not.

In practice, any orbit around a collinear libration point is dynamically unstable, meaning small departures from equilibrium grow exponentially over time. As a result, spacecraft in libration point orbits must use their propulsion systems to perform orbital stationkeeping.

Several missions have used Lissajous trajectories. ACE at Sun-Earth L1 and WMAP at Sun-Earth L2. On May 14, 2009, the European Space Agency (ESA) launched into space the Herschel and Planck observatories, both of which will use a Lissaujous orbit at at Sun-Earth L2. Also ESA's GAIA mission will use a Lissajous orbit at Sun-Earth L2 in the future.

References

  • Koon, W. S. (2006). Dynamical Systems, the Three-Body Problem, and Space Mission Design. {{cite book}}: Unknown parameter |coauthors= ignored (|author= suggested) (help)