Near optimal feedback guidance design and the planar restricted three-body problem

Joseph Dinius; Roberto Furfaro; Francesco Topputo; Scott Selnick

Near optimal feedback guidance design and the planar restricted three-body problem

Joseph Dinius, Roberto Furfaro, Francesco Topputo, Scott Selnick

Systems and Industrial Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

In this paper, we present the application of the ZEM/ZEV guidance algorithm to the planar restricted three-body problem (PR3BP). The ZEM/ZEV guidance law as a feedback guidance strategy is presented and applied to the PR3BP. The fuel optimal solution to the PR3BP for a transfer from GTO to L<inf>1</inf> in the Earth-Moon system is presented as a point for comparison, showing the near optimality of the closed-loop guidance approach. Challenges of the approach and strategies for implementation in spacecraft mission design are discussed.

Original language	English (US)
Title of host publication	Advances in the Astronautical Sciences
Publisher	Univelt Inc.
Pages	575-584
Number of pages	10
Volume	152
ISBN (Print)	9780877036111
State	Published - 2014
Event	24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States Duration: Jan 26 2014 → Jan 30 2014

Other

Other	24th AAS/AIAA Space Flight Mechanics Meeting, 2014
Country	United States
City	Mexico
Period	1/26/14 → 1/30/14

ASJC Scopus subject areas

Aerospace Engineering
Space and Planetary Science

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Cite this

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title = "Near optimal feedback guidance design and the planar restricted three-body problem",

abstract = "In this paper, we present the application of the ZEM/ZEV guidance algorithm to the planar restricted three-body problem (PR3BP). The ZEM/ZEV guidance law as a feedback guidance strategy is presented and applied to the PR3BP. The fuel optimal solution to the PR3BP for a transfer from GTO to L1 in the Earth-Moon system is presented as a point for comparison, showing the near optimality of the closed-loop guidance approach. Challenges of the approach and strategies for implementation in spacecraft mission design are discussed.",

author = "Joseph Dinius and Roberto Furfaro and Francesco Topputo and Scott Selnick",

year = "2014",

language = "English (US)",

isbn = "9780877036111",

volume = "152",

pages = "575--584",

booktitle = "Advances in the Astronautical Sciences",

publisher = "Univelt Inc.",

note = "24th AAS/AIAA Space Flight Mechanics Meeting, 2014 ; Conference date: 26-01-2014 Through 30-01-2014",

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AU - Dinius, Joseph

AU - Furfaro, Roberto

AU - Topputo, Francesco

AU - Selnick, Scott

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Y1 - 2014

N2 - In this paper, we present the application of the ZEM/ZEV guidance algorithm to the planar restricted three-body problem (PR3BP). The ZEM/ZEV guidance law as a feedback guidance strategy is presented and applied to the PR3BP. The fuel optimal solution to the PR3BP for a transfer from GTO to L1 in the Earth-Moon system is presented as a point for comparison, showing the near optimality of the closed-loop guidance approach. Challenges of the approach and strategies for implementation in spacecraft mission design are discussed.

AB - In this paper, we present the application of the ZEM/ZEV guidance algorithm to the planar restricted three-body problem (PR3BP). The ZEM/ZEV guidance law as a feedback guidance strategy is presented and applied to the PR3BP. The fuel optimal solution to the PR3BP for a transfer from GTO to L1 in the Earth-Moon system is presented as a point for comparison, showing the near optimality of the closed-loop guidance approach. Challenges of the approach and strategies for implementation in spacecraft mission design are discussed.

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M3 - Conference contribution

AN - SCOPUS:84940747394

SN - 9780877036111

VL - 152

SP - 575

EP - 584

BT - Advances in the Astronautical Sciences

PB - Univelt Inc.

T2 - 24th AAS/AIAA Space Flight Mechanics Meeting, 2014

Y2 - 26 January 2014 through 30 January 2014

ER -