Energy-optimal trajectory problems in relative motion solved via Theory of Functional Connections
Name:
TFC_Relative_Motion_Journal.pdf
Size:
987.0Kb
Format:
PDF
Description:
Final Accepted Manuscript
Affiliation
Systems & Industrial Engineering, University of ArizonaAerospace & Mechanical Engineering, University of Arizona
Issue Date
2021-02-04Keywords
Energy-optimal controlIndirect method
Least-squares
Spacecraft relative motion
Theory of functional connections
Metadata
Show full item recordPublisher
Elsevier LtdCitation
Drozd, K., Furfaro, R., Schiassi, E., Johnston, H., & Mortari, D. (2021). Energy-optimal trajectory problems in relative motion solved via Theory of Functional Connections. Acta Astronautica, 182, 361-382.Journal
Acta AstronauticaRights
© 2021 IAA. Published by Elsevier Ltd. All rights reserved.Collection Information
This item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.Abstract
In this paper, we present a new approach for solving a broad class of energy-optimal trajectory problems in relative motion using the recently developed Theory of Functional Connections (TFC). A total of four problem cases are considered and solved, i.e. rendezvous and intercept with fixed and free final time. Each problem is constrained and formulated using an indirect approach which casts the optimal trajectory problem as a system of linear or nonlinear two-point boundary value problems for the fixed and free final time cases, respectively. Using TFC, we convert each two-point boundary value problem into an unconstrained problem by analytically embedding the boundary constraints into a “constrained expression.” The latter includes a free-function that is expanded using Chebyshev polynomials with unknown coefficients. Regardless of the values of the unknown coefficients, the boundary constraints are satisfied and simple optimization schemes can be employed to numerically solve the problem (e.g. linear and nonlinear least-square methods). To validate the proposed approach, the TFC solutions are compared with solutions obtained via an analytical based method as well as direct and indirect numerical methods. In general, the proposed technique produces solutions to machine level accuracy. Additionally, for the cases tested, it is reported that computational run-time within the MATLAB implementation is lower than 28 and 300 ms for the fixed and free final time problems respectively. Consequently, the proposed methodology is potentially suitable for on-board generation of optimal trajectories in real-time.Note
24 month embargo; first published online 4 February 2021ISSN
0094-5765Version
Final accepted manuscriptae974a485f413a2113503eed53cd6c53
10.1016/j.actaastro.2021.01.031