Direct lunar descent optimisation by finite elements in time approach
Vasile, Massimiliano and Finzi, Amalia E. (2000) Direct lunar descent optimisation by finite elements in time approach. International Journal of Mechanics and Control, 1 (1). ISSN 1590-8844
PDF.
Filename: Vasile_M_Pure_Direct_lunar_descent_optimisation_by_finite_elements_in_time_approach_2000.pdf
Preprint Download (362kB) |
Abstract
In this paper a direct approach to trajectory optimisation, based on Finite Elements in Time (FET) discretisation is presented. Trajectory optimisation is performed combining the effectiveness and flexibility of Finite Elements in Time in solving complex boundary values problems with a common nonlinear programming algorithm. In order to avoid low accuracy proper to direct approaches, a mesh adaptivity strategy is implemented which exploits the ability of finite elements to represent both continuous and discontinuous functions. The effectiveness and accuracy of direct transcription by FET are proved by a selected number of sample problems. Finally an optimal landing manoeuvre is presented to show the power of the proposed approach in solving even complex and realistic problems.
ORCID iDs
Vasile, Massimiliano ORCID: https://orcid.org/0000-0001-8302-6465 and Finzi, Amalia E.;-
-
Item type: Article ID code: 41001 Dates: DateEventJanuary 2000PublishedSubjects: Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. AstronauticsDepartment: Faculty of Engineering > Mechanical and Aerospace Engineering Depositing user: Pure Administrator Date deposited: 03 Sep 2012 11:03 Last modified: 11 Nov 2024 10:13 URI: https://strathprints.strath.ac.uk/id/eprint/41001