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DESIGN AND CONTROL OF REPEAT GROUND TRACK ORBITS IN HIGH FIDELITY DYNAMICAL MODEL VIA HIGH ORDER POINCARÉ MAPPING

Armellin, Roberto, He, Yanchao and Xu, Ming (2019) DESIGN AND CONTROL OF REPEAT GROUND TRACK ORBITS IN HIGH FIDELITY DYNAMICAL MODEL VIA HIGH ORDER POINCARÉ MAPPING In: 29th AAS/AIAA Space Flight Mechanics Meeting, 13-17 January 2019, Ka'anapali, Maui, Hawaii.

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Abstract

A semi-analytical technique for both the design and control of repeat groundtrack (RGT) orbits in a high fidelity dynamical model, including non-conservative forces and accurate Earth orientation parameters, is introduced. The method is based on the use of high-order expansion of Poincaré maps to propagate forward in time regions of the phase space for one, or more, repeat cycles. This map provides the means to efficiently study the effect that an impulse, applied at the Poincaré section crossing, produces on the ground-track pattern, thus enabling highly accurate design and control. The approach is applied to the design and control of missions like TerraSAR-X, Landsat-8, SPOT-7, IRS-P6, and UoSAT-12.

Item Type: Conference or Workshop Item (Conference Paper)
Divisions : Faculty of Engineering and Physical Sciences > Electronic Engineering
Authors :
NameEmailORCID
Armellin, Robertor.armellin@surrey.ac.uk
He, Yanchao
Xu, Ming
Date : 8 February 2019
Copyright Disclaimer : Copyright 2019 by AMERICAN ASTRONAUTICAL SOCIETY
Depositing User : Diane Maxfield
Date Deposited : 26 Feb 2019 13:04
Last Modified : 26 Feb 2019 13:04
URI: http://epubs.surrey.ac.uk/id/eprint/850576

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