A Two-Level Optimization Method for Hypersonic Periodic Cruise Trajectory

Periodic cruise has the potential to improve the fuel-saving efficiency of hypersonic cruise vehicle but is difficult to optimize. In this paper, a two-level optimization method for the trajectory of periodic cruise is proposed. Due to that the periodic cruise trajectory can be divided into an accel...

Full description

Saved in:
Bibliographic Details
Main Authors: Hesong Li, Yi Wang, Yunfan Zhou, Shangcheng Xu, Dan Su
Format: Article
Language:English
Published: Wiley 2021-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2021/9975007
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1832546016446906368
author Hesong Li
Yi Wang
Yunfan Zhou
Shangcheng Xu
Dan Su
author_facet Hesong Li
Yi Wang
Yunfan Zhou
Shangcheng Xu
Dan Su
author_sort Hesong Li
collection DOAJ
description Periodic cruise has the potential to improve the fuel-saving efficiency of hypersonic cruise vehicle but is difficult to optimize. In this paper, a two-level optimization method for the trajectory of periodic cruise is proposed. Due to that the periodic cruise trajectory can be divided into an acceleration phase where engine works and a glide phase where engine is off, the two-level optimization method is proposed to optimize the trajectory in each phase by the corresponding level. In the first level, Downhill Simplex Method (DSM) is employed to find an optimal angle of attack in the acceleration phase. Subsequently, the optimal trajectory in glide phase is obtained by the Pseudo-Spectral Method (PSM) in the second optimization level. Numerical results demonstrate the effectiveness of the proposed method. Finally, through comparing with steady-state cruise, it is concluded that periodic cruise makes full use of the change of atmospheric density and lift-drag ratio; thus, fuel saving is achieved.
format Article
id doaj-art-c59ab72c5cd14541a1a0f48f96da5db1
institution Kabale University
issn 1687-5966
1687-5974
language English
publishDate 2021-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-c59ab72c5cd14541a1a0f48f96da5db12025-02-03T07:24:12ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742021-01-01202110.1155/2021/99750079975007A Two-Level Optimization Method for Hypersonic Periodic Cruise TrajectoryHesong Li0Yi Wang1Yunfan Zhou2Shangcheng Xu3Dan Su4College of Aerospace Science, National University of Defense Technology, Changsha 410073, ChinaCollege of Aerospace Science, National University of Defense Technology, Changsha 410073, ChinaCollege of Aerospace Science, National University of Defense Technology, Changsha 410073, ChinaCollege of Aerospace Science, National University of Defense Technology, Changsha 410073, ChinaCollege of Aerospace Science, National University of Defense Technology, Changsha 410073, ChinaPeriodic cruise has the potential to improve the fuel-saving efficiency of hypersonic cruise vehicle but is difficult to optimize. In this paper, a two-level optimization method for the trajectory of periodic cruise is proposed. Due to that the periodic cruise trajectory can be divided into an acceleration phase where engine works and a glide phase where engine is off, the two-level optimization method is proposed to optimize the trajectory in each phase by the corresponding level. In the first level, Downhill Simplex Method (DSM) is employed to find an optimal angle of attack in the acceleration phase. Subsequently, the optimal trajectory in glide phase is obtained by the Pseudo-Spectral Method (PSM) in the second optimization level. Numerical results demonstrate the effectiveness of the proposed method. Finally, through comparing with steady-state cruise, it is concluded that periodic cruise makes full use of the change of atmospheric density and lift-drag ratio; thus, fuel saving is achieved.http://dx.doi.org/10.1155/2021/9975007
spellingShingle Hesong Li
Yi Wang
Yunfan Zhou
Shangcheng Xu
Dan Su
A Two-Level Optimization Method for Hypersonic Periodic Cruise Trajectory
International Journal of Aerospace Engineering
title A Two-Level Optimization Method for Hypersonic Periodic Cruise Trajectory
title_full A Two-Level Optimization Method for Hypersonic Periodic Cruise Trajectory
title_fullStr A Two-Level Optimization Method for Hypersonic Periodic Cruise Trajectory
title_full_unstemmed A Two-Level Optimization Method for Hypersonic Periodic Cruise Trajectory
title_short A Two-Level Optimization Method for Hypersonic Periodic Cruise Trajectory
title_sort two level optimization method for hypersonic periodic cruise trajectory
url http://dx.doi.org/10.1155/2021/9975007
work_keys_str_mv AT hesongli atwoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT yiwang atwoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT yunfanzhou atwoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT shangchengxu atwoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT dansu atwoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT hesongli twoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT yiwang twoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT yunfanzhou twoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT shangchengxu twoleveloptimizationmethodforhypersonicperiodiccruisetrajectory
AT dansu twoleveloptimizationmethodforhypersonicperiodiccruisetrajectory