Searched for: mods_originInfo_publisher_s%3A%22Univelt%255C+Inc.%22
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Vakaet, Christophe (author), Menicucci, A. (author)
CubeSat based constellations are limited by launch opportunities, manoeuvring, and reliability. In this paper, an approach is proposed to determine the performance of a constellation, using different deployment strategies. Due to low maneuverability and limited launch options, CubeSats require deployment strategies that determine the optimal...
conference paper 2018
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Uludag, M.S. (author), Speretta, S. (author), Gill, E.K.A. (author), Bouwmeester, J. (author), Pérez Soriano, T. (author)
Due to strict constraint regarding the volume of a PocketQube (50x50x50 mm) it is crucial to reduce the space that is consumed by the satellite bus subsystems. This paper focuses on a new architecture for the electrical subsystem in order to reduce its volume and increase the usage of empty surfaces inside the satellite. This increment in volume...
conference paper 2017
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Heiligers, M.J. (author), Scheeres, Daniel J. (author)
While SRP is often considered an undesirable effect, especially for missions to small bodies like asteroids and binary asteroid systems, this paper utilizes the SRP on a solar sail to generate artificial equilibrium points (AEPs) and displaced periodic orbits in these systems. While the solar sail dynamics for the single asteroid case are...
conference paper 2017