Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles
Guidance with traditional trajectory correction scheme usually starts from the trajectory apex time to reduce drag penalties early in flight; however, this method cannot get the max trajectory correction capability of canards according to our analysis. This paper presents an optimized trajectory cor...
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Format: | Article |
Language: | English |
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Wiley
2015-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2015/618458 |
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author | Yongwei Zhang Min Gao Suochang Yang Dan Fang |
author_facet | Yongwei Zhang Min Gao Suochang Yang Dan Fang |
author_sort | Yongwei Zhang |
collection | DOAJ |
description | Guidance with traditional trajectory correction scheme usually starts from the trajectory apex time to reduce drag penalties early in flight; however, this method cannot get the max trajectory correction capability of canards according to our analysis. This paper presents an optimized trajectory correction scheme by taking different control phases of canards in ballistic ascending segment and ballistic descending segment. Simulation indicates that the optimized trajectory correction can improve the trajectory correction capability greatly. The result of an example trajectory and Monte Carlo simulations with the predictive guidance law and the trajectory tracking guidance law testifies the effectiveness of the optimized trajectory correction scheme. |
format | Article |
id | doaj-art-b821b89e09484d828524e3a46c6f0ebe |
institution | Kabale University |
issn | 1687-5966 1687-5974 |
language | English |
publishDate | 2015-01-01 |
publisher | Wiley |
record_format | Article |
series | International Journal of Aerospace Engineering |
spelling | doaj-art-b821b89e09484d828524e3a46c6f0ebe2025-02-03T01:08:06ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742015-01-01201510.1155/2015/618458618458Optimization of Trajectory Correction Scheme for Guided Mortar ProjectilesYongwei Zhang0Min Gao1Suochang Yang2Dan Fang3Electronic Engineering Department, Shijiazhuang Mechanical Engineering College, No. 97 Heping West Road, Shijiazhuang, Hebei 050003, ChinaElectronic Engineering Department, Shijiazhuang Mechanical Engineering College, No. 97 Heping West Road, Shijiazhuang, Hebei 050003, ChinaElectronic Engineering Department, Shijiazhuang Mechanical Engineering College, No. 97 Heping West Road, Shijiazhuang, Hebei 050003, ChinaElectronic Engineering Department, Shijiazhuang Mechanical Engineering College, No. 97 Heping West Road, Shijiazhuang, Hebei 050003, ChinaGuidance with traditional trajectory correction scheme usually starts from the trajectory apex time to reduce drag penalties early in flight; however, this method cannot get the max trajectory correction capability of canards according to our analysis. This paper presents an optimized trajectory correction scheme by taking different control phases of canards in ballistic ascending segment and ballistic descending segment. Simulation indicates that the optimized trajectory correction can improve the trajectory correction capability greatly. The result of an example trajectory and Monte Carlo simulations with the predictive guidance law and the trajectory tracking guidance law testifies the effectiveness of the optimized trajectory correction scheme.http://dx.doi.org/10.1155/2015/618458 |
spellingShingle | Yongwei Zhang Min Gao Suochang Yang Dan Fang Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles International Journal of Aerospace Engineering |
title | Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles |
title_full | Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles |
title_fullStr | Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles |
title_full_unstemmed | Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles |
title_short | Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles |
title_sort | optimization of trajectory correction scheme for guided mortar projectiles |
url | http://dx.doi.org/10.1155/2015/618458 |
work_keys_str_mv | AT yongweizhang optimizationoftrajectorycorrectionschemeforguidedmortarprojectiles AT mingao optimizationoftrajectorycorrectionschemeforguidedmortarprojectiles AT suochangyang optimizationoftrajectorycorrectionschemeforguidedmortarprojectiles AT danfang optimizationoftrajectorycorrectionschemeforguidedmortarprojectiles |