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A Comparative Study of Displaced Non-Keplerian Orbits with Impulsive and Continuous Thrust

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Simo, Jules ORCID: 0000-0002-1489-5920 (2017) A Comparative Study of Displaced Non-Keplerian Orbits with Impulsive and Continuous Thrust. In: Spaceflight Mechanics 2017: Proceedings of the 27th AAS/AIAA Space Flight Mechanics Meeting. Univelt, Inc., San Diego, California, pp. 2531-2552.

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Official URL: http://www.univelt.com/book=6200

Abstract

A study of novel families of highly non-Keplerian orbits (NKO) for spacecraft utilizing either solar sail or solar electric propulsion (SEP) at linear order are investigated in the circular restricted three-body problem (CRTBP). In addition to a detailed investigation of the dynamics and control of highly NKO, effort will be devoted to develop a strategy that uses maneuvers executed impulsively at discrete time intervals. Thus, impulse control is investigated as a means of generating displaced orbits. In order to compare the continuous thrust and impulse control orbits, linearized equations of motion will be considered for small displacements. The requirements for impulse control and continuous thrust for different values of out-of-plane distance are presented.

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Item Type:	Book Section
Additional Information:	This paper was originally presented at the 27th AAS/AIAA Space Flight Mechanics Meeting, held February 5-9, 2017 San Antonio, Texas, U.S.A. and was originally published in the American Astronautical Society (AAS) publication Spaceflight Mechanics 2017, edited by J. W. McMahon, Y. Guo, F. A. Leve and J. A. Sims, AAS Advances in the Astronautical Sciences, Volume 160, pp. 2531-2552 (Copyright ©2017 by American Astronautical Society Publications Office, P.O. Box 28130, San Diego, CA 92198, U.S.A.; Web Site: http://www.univelt.com
Creators (Authors or editors):	Creators Email ORCID Simo, Jules jsimo@uclan.ac.uk orcid.org/0000-0002-1489-5920
Uncontrolled Keywords (separate with ;):	Impulse control; Continuous thrust; Hybrid propulsion; Space missions; Non-Keplerian orbits; Circular restricted three-body problem
Subjects:	H - Engineering > H300 - Mechanical engineering H - Engineering > H310 - Dynamics H - Engineering > H400 - Aerospace engineering H - Engineering > H410 - Aeronautical engineering H - Engineering > H420 - Astronautical engineering H - Engineering > H441 - Flight mechanics H - Engineering > H450 - Propulsion systems H - Engineering > H620 - Electrical engineering H - Engineering > H650 - Systems engineering H - Engineering > H660 - Control systems H - Engineering > H670 - Robotics & cybernetics H - Engineering > H730 - Mechatronics
Schools:	School of Engineering and Computing > Engineering, Construction, Maths and Physics
ID Code:	23868
Depositing User ID:	Jules Simo
Date Deposited:	20 Aug 2018 10:30
Last Modified:	01 May 2024 08:36

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A Comparative Study of Displaced Non-Keplerian Orbits with Impulsive and Continuous Thrust

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