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 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.

Original language	English (US)
Title of host publication	Advances In The Astronautical Sciences
Editors	Donald L. Mackison, Ossama Abdelkhalik, Roby S. Wilson, Renato Zanetti
Publisher	Univelt Inc.
Pages	575-584
Number of pages	10
ISBN (Electronic)	9780877036111
State	Published - 2014
Event	24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States Duration: Jan 26 2014 → Jan 30 2014

Publication series

Name	Advances in the Astronautical Sciences
Volume	152
ISSN (Print)	0065-3438

Other

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

ASJC Scopus subject areas

Aerospace Engineering
Space and Planetary Science

Cite this

Near optimal feedback guidance design and the planar restricted three-body problem. / Dinius, Joseph; Furfaro, Roberto; Topputo, Francesco et al.
Advances In The Astronautical Sciences. ed. / Donald L. Mackison; Ossama Abdelkhalik; Roby S. Wilson; Renato Zanetti. Univelt Inc., 2014. p. 575-584 (Advances in the Astronautical Sciences; Vol. 152).

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

Dinius, J, Furfaro, R, Topputo, F & Selnick, S 2014, Near optimal feedback guidance design and the planar restricted three-body problem. in DL Mackison, O Abdelkhalik, RS Wilson & R Zanetti (eds), Advances In The Astronautical Sciences. Advances in the Astronautical Sciences, vol. 152, Univelt Inc., pp. 575-584, 24th AAS/AIAA Space Flight Mechanics Meeting, 2014, Mexico, United States, 1/26/14.

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ER -

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

Abstract

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ASJC Scopus subject areas

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