Computational guidance using sparse Gauss-Hermite quadrature differential dynamic programming
| dc.contributor.author | He, Shaoming | |
| dc.contributor.author | Shin, Hyo-Sang | |
| dc.contributor.author | Tsourdos, Antonios | |
| dc.date.accessioned | 2020-02-05T10:41:15Z | |
| dc.date.available | 2020-02-05T10:41:15Z | |
| dc.date.issued | 2019-11-25 | |
| dc.description.abstract | This paper proposes a new computational guidance algorithm using differential dynamic programming and sparse Gauss-Hermite quadrature rule. By the application of sparse Gauss-Hermite quadrature rule, numerical differentiation in the calculation of Hessian matrices and gradients in differential dynamic programming is avoided. Based on the new differential dynamic programming approach developed, a three-dimensional computational algorithm is proposed to control the impact angle and impact time for an air-to-surface interceptor. Extensive numerical simulations are performed to show the effectiveness of the proposed approach. | en_UK |
| dc.identifier.citation | He S, Shin H-S, Tsourdos A. (2019) Computational guidance using sparse Gauss-Hermite quadrature differential dynamic programming. IFAC-PapersOnLine, Volume 52, Issue 12, 2019, pp. 13-18 | en_UK |
| dc.identifier.issn | 2405-8963 | |
| dc.identifier.uri | https://doi.org/10.1016/j.ifacol.2019.11.062 | |
| dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/15091 | |
| dc.language.iso | en | en_UK |
| dc.publisher | Elsevier | en_UK |
| dc.rights | Attribution-NonCommercial 4.0 International | * |
| dc.rights.uri | http://creativecommons.org/licenses/by-nc/4.0/ | * |
| dc.subject | Computational guidance | en_UK |
| dc.subject | Differential dynamic programming | en_UK |
| dc.subject | Sparse Gauss-Hermite quadrature | en_UK |
| dc.subject | Impact angle | en_UK |
| dc.subject | Impact time | en_UK |
| dc.title | Computational guidance using sparse Gauss-Hermite quadrature differential dynamic programming | en_UK |
| dc.type | Article | en_UK |