2014
DOI: 10.1063/1.4904574
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The mechanics of motorised momentum exchange tethers when applied to active debris removal from LEO

Abstract: Abstract. The concept of momentum exchange when applied to space tethers for propulsion is well established, and a considerable body of literature now exists on the on-orbit modelling, the dynamics, and also the control of a large range of tether system applications. The authors consider here a new application for the Motorised Momentum Exchange Tether by highlighting three key stages of development leading to a conceptualisation that can subsequently be developed into a technology for Active Debris Removal. T… Show more

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Cited by 2 publications
(1 citation statement)
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“…The deployment dynamics of a tethered system is highly nonlinear [60][61] [62] and the Coriolis accelerations acting on the tip masses leads to a configuration of the tethered system with libration amplitudes that are typically in the range 40°-50° if uncontrolled [63]. Consequently, the first step in the design of a deployment trajectory is to compute tether length and velocity time profiles that bring the system from given initial conditions to a small libration amplitude at the end of the deployment maneuver.…”
Section: Software Tools For Edt 41 Deployment Trajectory Design Toolsmentioning
confidence: 99%
“…The deployment dynamics of a tethered system is highly nonlinear [60][61] [62] and the Coriolis accelerations acting on the tip masses leads to a configuration of the tethered system with libration amplitudes that are typically in the range 40°-50° if uncontrolled [63]. Consequently, the first step in the design of a deployment trajectory is to compute tether length and velocity time profiles that bring the system from given initial conditions to a small libration amplitude at the end of the deployment maneuver.…”
Section: Software Tools For Edt 41 Deployment Trajectory Design Toolsmentioning
confidence: 99%