2021
DOI: 10.1016/j.asr.2020.09.034
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LISA: Heliocentric formation design for the laser interferometer space antenna mission

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Cited by 26 publications
(16 citation statements)
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“…Accounting for the sole influence of the Sun, the computation of their positions and velocities reduces to a two-body problem, which can be solved semi-analytically [18,19]. A more realistic approach uses a set of orbits computed using numerical integration (which includes the influence of the more massive objects in the Solar System) optimized for a given set of constraints, such as minimizing the motion of the spacecraft relative to one another [19][20][21].…”
Section: Interferometric Measurementsmentioning
confidence: 99%
See 1 more Smart Citation
“…Accounting for the sole influence of the Sun, the computation of their positions and velocities reduces to a two-body problem, which can be solved semi-analytically [18,19]. A more realistic approach uses a set of orbits computed using numerical integration (which includes the influence of the more massive objects in the Solar System) optimized for a given set of constraints, such as minimizing the motion of the spacecraft relative to one another [19][20][21].…”
Section: Interferometric Measurementsmentioning
confidence: 99%
“…The factor ḋij (t)D ij ν j is often referred to as the Doppler shift, and is proportional to the time derivative of the light TT. Figure 2 show the time variations of such quantities for realistic orbits [20,21], of the order of 10 −8 (or 3 m s −1 ). The inter-spacecraft interferometer mixes the local and distant beams.…”
Section: Interferometric Measurementsmentioning
confidence: 99%
“…DSSs are comprised of a large number of spacecraft that cooperate with one another to accomplish a specific mission objective [ 4 ]. In some circumstances, DSSs combine to generate a sensory system that would be impossible to create on a monolithic platform [ 5 , 6 ]. In other configurations, they use distributed measurements to extract data on the spatial and temporal consequences of phenomena that are far larger than what a single spacecraft can observe due to limited swath width and duty cycle [ 7 , 8 ].…”
Section: Introductionmentioning
confidence: 99%
“…The primary obstacle is the extremely lengthy baseline distance, making communication and measurement difficult. For sufficient detection sensitivity, gravitational wave detectors in space need baseline distances of a few dozen kilometers or possibly millions of kilometers [ 10 , 11 ]. Nevertheless, such lengths would make it challenging to implement formation control methods that depend on relative state measurements.…”
Section: Introductionmentioning
confidence: 99%