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The bodies of a binary asteroid system have small masses and irregular shapes. In the vicinity of such a system, perturbations, like the Solar Radiation Pressure (SRP), can not be neglected when designing spacecraft trajectories. This paper shows how to integrate the SRP in the design of the trajectory of a spacecraft in that context, especially about the L1 Lagrangian point of the system.

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This page is a summary of: Solar Radiation Pressure–Compatible Trajectories in the Vicinity of a Binary Asteroid, Journal of Guidance Control and Dynamics, January 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004007.
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