Autonomous orbit determination and navigation for formations of CubeSats beyond LEO
Vasile, Massimiliano and Torre, Francesco and Serra, Romain and Grey, Stuart (2017) Autonomous orbit determination and navigation for formations of CubeSats beyond LEO. In: 9th International Workshop on Satellite Constellations and Formation Flying, 2017-06-19 - 2017-06-21, University of Colorado Boulder.
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Abstract
This paper investigates the use of the Time Of Arrival (TOA) and Doppler shift to allow a small formation of CubeSats to navigate beyond low Earth orbit (LEO). The idea is to use a one way communication, from one or more ground station to two or more CubeSats, to reconstruct an estimation of the position and velocity of the formation with respect to Earth. The paper considers the use of the difference in TOA and Doppler measurements to mitigate the error introduced by the onboard clock. These measurements are combined with inter-satellite distance and velocity measurements based on a two-way communication between pairs of spacecraft. The paper will provide an estimation of the error in position and velocity that can be obtained by a combination of these measurements. The reference case for these analyses will be a mission to the Moon.
ORCID iDs
Vasile, Massimiliano ORCID: https://orcid.org/0000-0001-8302-6465, Torre, Francesco ORCID: https://orcid.org/0000-0003-0278-1405, Serra, Romain and Grey, Stuart ORCID: https://orcid.org/0000-0001-9274-0601;-
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Item type: Conference or Workshop Item(Paper) ID code: 63264 Dates: DateEvent19 June 2017Published9 January 2017AcceptedSubjects: Technology > Motor vehicles. Aeronautics. Astronautics Department: Faculty of Engineering > Mechanical and Aerospace Engineering
Strategic Research Themes > Ocean, Air and SpaceDepositing user: Pure Administrator Date deposited: 13 Feb 2018 14:29 Last modified: 11 Nov 2024 16:52 URI: https://strathprints.strath.ac.uk/id/eprint/63264