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Lissajous orbit

Quasi-periodic orbital trajectory

Quasi-periodic orbital trajectory

In orbital mechanics, a Lissajous orbit (), named after Jules Antoine Lissajous, is a quasi-periodic orbital trajectory that an object can follow around a Lagrangian point of a three-body system with minimal propulsion. Lyapunov orbits around a Lagrangian 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 usually not.

In practice, any orbits around Lagrangian points , , or are dynamically unstable, meaning small departures from equilibrium grow over time. As a result, spacecraft in these Lagrangian point orbits must use their propulsion systems to perform orbital station-keeping. Although they are not perfectly stable, a modest effort of station keeping keeps a spacecraft in a desired Lissajous orbit for a long time.

In the absence of other influences, orbits about Lagrangian points and are dynamically stable so long as the ratio of the masses of the two main objects is greater than about 25. The natural dynamics keep the spacecraft (or natural celestial body) in the vicinity of the Lagrangian point without use of a propulsion system, even when slightly perturbed from equilibrium. These orbits can however be destabilized by other nearby massive objects. For example, orbits around the and points in the Earth–Moon system can last only a few million years instead of billions because of perturbations by the other planets in the Solar System.

Spacecraft using Lissajous orbits

Main article: Spacecraft using Lissajous orbits

Several missions have used Lissajous orbits: ACE at Sun–Earth L1, SOHO at Sun–Earth L1, DSCOVR at Sun–Earth L1, WMAP at Sun–Earth L2, and also the Genesis mission collecting solar particles at L1. On 14 May 2009, the European Space Agency (ESA) launched into space the Herschel and Planck observatories, both of which use Lissajous orbits at Sun–Earth L2. | access-date = 2006-05-15}}

ESA's Gaia mission also uses a Lissajous orbit at Sun–Earth L2.{{cite web | access-date = 2006-05-15 | archive-url = https://web.archive.org/web/20170318200526/http://sci2.esa.int/interactive/media/flashes/5_5_1.htm | archive-date = 2017-03-18 | url-status = dead

In 2011, NASA transferred two of its THEMIS spacecraft from Earth orbit to Lunar orbit by way of Earth–Moon L1 and L2 Lissajous orbits.

In June 2018, Queqiao, the relay satellite for China's Chang'e 4 lunar lander mission, entered orbit around Earth-Moon L2.

Fictional appearances

In the 2005 science fiction novel Sunstorm by Arthur C. Clarke and Stephen Baxter, a huge shield is constructed in space to protect the Earth from a deadly solar storm. The shield is described to have been in a Lissajous orbit at . In the story a group of wealthy and powerful people shelter opposite the shield at so as to be protected from the solar storm by the shield, the Earth and the Moon.

In the 2017 science fiction novel Artemis by Andy Weir, a Lissajous orbit is used as a transfer point for routine travel to and from the Moon.

Notes

References

References

  1. (14 June 2009). "ESA Science & Technology: Orbit/Navigation". [[European Space Agency]].
  2. "A230242 – Decimal expansion of (25+3*sqrt(69))/2".
  3. Vallado, David A.. (2007). "Fundamentals of Astrodynamics and Applications". Springer New York.
  4. (2008). "Solar and planetary destabilization of the Earth–Moon triangular Lagrangian points". [[Icarus (journal).
  5. "ACE Mission".
  6. Bergin, Chris. (2015-02-11). "SpaceX Falcon 9 successfully launches the DSCOVR spacecraft".
  7. "WMAP Observatory: Trajectory and Orbit".
  8. "Genesis: Search for Origins {{!}} JPL {{!}} NASA".
  9. [http://www.igpp.ucla.edu/public/THEMIS/SCI/Pubs/artemis/artemis_woodward.pdf ARTEMIS: The First Mission to the Lunar Libration Orbits]
  10. (14 June 2018). "Chang'e-4 relay satellite enters halo orbit around Earth-Moon L2, microsatellite in lunar orbit".
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three-body-orbits trigonometry lagrangian-mechanics
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