Orbit Design and Optimization for the Gravitational Wave Detection of LISA

Details Orbit Design and Optimization for the Gravitational Wave Detection of LISA Orbit Design and Optimization for the Gravitational Wave Detection of LISA

Apr 2010

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2010gras.conf...78x&link_type=abstract

GRAVITATION AND ASTROPHYSICS. Proceedings of the Ninth Asia-Pacific International Conference. Held 29 June-2 July 2009 in Wuhan,

Astronomy and Astrophysics

Astrophysics

Co-Orbital Restricted Problem, Orbit Design, Orbit Optimization

Scientific paper

The Laser Interferometer Space Antenna (LISA) is a joint ESA-NASA mission for detecting low-frequency gravitational waves, by using accurate distance measurements with laser interferometry between three spacecrafts, which will be launched around 2018 and one year later reach their operational orbits around the Sun. In order to operate successfully, it is crucial for the constellation of the three spacecrafts to have extremely high stability. Based on the study of operational orbits for a 2015 launch, we designed the operational orbits of beginning epoch on 2019-03-01, analyzed the acceptable error range of the injection, and introduced the method of orbit design and optimization.

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