Multi-Revolution Perturbed Lambert’s Problem

Armellin, Roberto, Gondelach, David and San Juan, JF (2018) Multi-Revolution Perturbed Lambert’s Problem In: 28th AIAA/AAS Space Flight Mechanics Meeting, 8 - 12 January 2018, Kissimmee, Florida.

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Abstract

The solution of multiple-revolution perturbed Lambert problems is a challenging task due to the high sensitivity of the final state to variations of the initial velocity. In this work two different solvers based on high order Taylor expansions and an analytical solution of the J2 problem are presented. In addition, an iteration-less procedure is developed to refine the solutions in a dynamical model that includes J2 − J4 perturbations. The properties of the proposed approached are tested against transfers with hundreds of revolutions including those required to solve the Global Trajectory Optimisation Competition 9.

Item Type:	Conference or Workshop Item (Conference Paper)
Divisions :	Faculty of Engineering and Physical Sciences > Electronic Engineering
Authors :	Name Email ORCID Armellin, Roberto r.armellin@surrey.ac.uk Gondelach, David d.gondelach@surrey.ac.uk San Juan, JF
Date :	8 February 2018
DOI :	10.2514/6.2018-1968
Copyright Disclaimer :	Copyright 2018 American Institute of Aeronautics and Astronautics
Depositing User :	Melanie Hughes
Date Deposited :	21 Nov 2017 15:37
Last Modified :	16 Jan 2019 19:04
URI:	http://epubs.surrey.ac.uk/id/eprint/844973

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