Three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint
Studying a guidance law, which can intercepts not only high-speed targets, but also low-speed targets with impact angle constrains, is a challenging task. In this paper, a new guidance law called united biased proportional navigation (UBPN) is proposed. The guidance law uses time-varying bias and na...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Liang Yan [verfasserIn] |
|---|
| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2015 |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: Proceedings of the Institution of Mechanical Engineers / G - London : Inst., 1989, 229(2015), 6, Seite 1013 |
|---|---|
| Übergeordnetes Werk: |
volume:229 ; year:2015 ; number:6 ; pages:1013 |
| Links: |
|---|
| DOI / URN: |
10.1177/0954410014543714 |
|---|
| Katalog-ID: |
OLC1958296384 |
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| 520 | |a Studying a guidance law, which can intercepts not only high-speed targets, but also low-speed targets with impact angle constrains, is a challenging task. In this paper, a new guidance law called united biased proportional navigation (UBPN) is proposed. The guidance law uses time-varying bias and navigation ratio, and incorporates the advantages of head-on and head-pursuit engagement. UBPN with positive time-varying navigation ratio can intercept low-speed targets which is a head-on engagement, while with negative time-varying navigation ratio can intercept high-speed targets, which is a head-pursuit engagement. To begin with, planar UBPN guidance law is proposed and exact time-varying bias is derived. Moreover, the solution to the singularity in time-varying navigation ratio is given. Secondly, in order to realize the guidance law in three-dimensional space, we derive the relation between two-dimensional acceleration and three-dimensional acceleration, and also give the solution for calculating the impact angle from two-dimensional surface into three-dimensional space. Finally, the simulation results of UBPN compared with proportional navigation, retro-proportional navigation, and bias proportional navigation guidance law are shown. It is demonstrated that the miss distance and impact angle error can meet the guidance law requirements. Capture region of UBPN is given by simulation, which indicates that it is almost two times than that of the guidance law in the head-on engagement for interception of high-speed target. | ||
| 650 | 4 | |a Aerospace engineering | |
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10.1177/0954410014543714 doi PQ20160617 (DE-627)OLC1958296384 (DE-599)GBVOLC1958296384 (PRQ)c2466-4a92799babf4dee088b0f295420f36a3619418ea8e2b00d95ab5a81d858b33560 (KEY)0178350520150000229000601013threedimensionalunitedbiasedproportionalnavigation DE-627 ger DE-627 rakwb eng 380 ZDB Liang Yan verfasserin aut Three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint 2015 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier Studying a guidance law, which can intercepts not only high-speed targets, but also low-speed targets with impact angle constrains, is a challenging task. In this paper, a new guidance law called united biased proportional navigation (UBPN) is proposed. The guidance law uses time-varying bias and navigation ratio, and incorporates the advantages of head-on and head-pursuit engagement. UBPN with positive time-varying navigation ratio can intercept low-speed targets which is a head-on engagement, while with negative time-varying navigation ratio can intercept high-speed targets, which is a head-pursuit engagement. To begin with, planar UBPN guidance law is proposed and exact time-varying bias is derived. Moreover, the solution to the singularity in time-varying navigation ratio is given. Secondly, in order to realize the guidance law in three-dimensional space, we derive the relation between two-dimensional acceleration and three-dimensional acceleration, and also give the solution for calculating the impact angle from two-dimensional surface into three-dimensional space. Finally, the simulation results of UBPN compared with proportional navigation, retro-proportional navigation, and bias proportional navigation guidance law are shown. It is demonstrated that the miss distance and impact angle error can meet the guidance law requirements. Capture region of UBPN is given by simulation, which indicates that it is almost two times than that of the guidance law in the head-on engagement for interception of high-speed target. Aerospace engineering Dimensional analysis Mathematical problems Simulation High speed Navigation systems Acceleration Ji-Guang Zhao oth Huai-Rong Shen oth Yuan Li oth Enthalten in Proceedings of the Institution of Mechanical Engineers / G London : Inst., 1989 229(2015), 6, Seite 1013 (DE-627)130823449 (DE-600)1015042-0 (DE-576)023064404 0954-4100 nnns volume:229 year:2015 number:6 pages:1013 http://dx.doi.org/10.1177/0954410014543714 Volltext http://search.proquest.com/docview/1676467304 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_2006 GBV_ILN_4046 AR 229 2015 6 1013 |
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Three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint |
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Three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint |
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Liang Yan |
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Proceedings of the Institution of Mechanical Engineers / G |
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10.1177/0954410014543714 |
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three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint |
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Three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint |
| abstract |
Studying a guidance law, which can intercepts not only high-speed targets, but also low-speed targets with impact angle constrains, is a challenging task. In this paper, a new guidance law called united biased proportional navigation (UBPN) is proposed. The guidance law uses time-varying bias and navigation ratio, and incorporates the advantages of head-on and head-pursuit engagement. UBPN with positive time-varying navigation ratio can intercept low-speed targets which is a head-on engagement, while with negative time-varying navigation ratio can intercept high-speed targets, which is a head-pursuit engagement. To begin with, planar UBPN guidance law is proposed and exact time-varying bias is derived. Moreover, the solution to the singularity in time-varying navigation ratio is given. Secondly, in order to realize the guidance law in three-dimensional space, we derive the relation between two-dimensional acceleration and three-dimensional acceleration, and also give the solution for calculating the impact angle from two-dimensional surface into three-dimensional space. Finally, the simulation results of UBPN compared with proportional navigation, retro-proportional navigation, and bias proportional navigation guidance law are shown. It is demonstrated that the miss distance and impact angle error can meet the guidance law requirements. Capture region of UBPN is given by simulation, which indicates that it is almost two times than that of the guidance law in the head-on engagement for interception of high-speed target. |
| abstractGer |
Studying a guidance law, which can intercepts not only high-speed targets, but also low-speed targets with impact angle constrains, is a challenging task. In this paper, a new guidance law called united biased proportional navigation (UBPN) is proposed. The guidance law uses time-varying bias and navigation ratio, and incorporates the advantages of head-on and head-pursuit engagement. UBPN with positive time-varying navigation ratio can intercept low-speed targets which is a head-on engagement, while with negative time-varying navigation ratio can intercept high-speed targets, which is a head-pursuit engagement. To begin with, planar UBPN guidance law is proposed and exact time-varying bias is derived. Moreover, the solution to the singularity in time-varying navigation ratio is given. Secondly, in order to realize the guidance law in three-dimensional space, we derive the relation between two-dimensional acceleration and three-dimensional acceleration, and also give the solution for calculating the impact angle from two-dimensional surface into three-dimensional space. Finally, the simulation results of UBPN compared with proportional navigation, retro-proportional navigation, and bias proportional navigation guidance law are shown. It is demonstrated that the miss distance and impact angle error can meet the guidance law requirements. Capture region of UBPN is given by simulation, which indicates that it is almost two times than that of the guidance law in the head-on engagement for interception of high-speed target. |
| abstract_unstemmed |
Studying a guidance law, which can intercepts not only high-speed targets, but also low-speed targets with impact angle constrains, is a challenging task. In this paper, a new guidance law called united biased proportional navigation (UBPN) is proposed. The guidance law uses time-varying bias and navigation ratio, and incorporates the advantages of head-on and head-pursuit engagement. UBPN with positive time-varying navigation ratio can intercept low-speed targets which is a head-on engagement, while with negative time-varying navigation ratio can intercept high-speed targets, which is a head-pursuit engagement. To begin with, planar UBPN guidance law is proposed and exact time-varying bias is derived. Moreover, the solution to the singularity in time-varying navigation ratio is given. Secondly, in order to realize the guidance law in three-dimensional space, we derive the relation between two-dimensional acceleration and three-dimensional acceleration, and also give the solution for calculating the impact angle from two-dimensional surface into three-dimensional space. Finally, the simulation results of UBPN compared with proportional navigation, retro-proportional navigation, and bias proportional navigation guidance law are shown. It is demonstrated that the miss distance and impact angle error can meet the guidance law requirements. Capture region of UBPN is given by simulation, which indicates that it is almost two times than that of the guidance law in the head-on engagement for interception of high-speed target. |
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Three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint |
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http://dx.doi.org/10.1177/0954410014543714 http://search.proquest.com/docview/1676467304 |
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Ji-Guang Zhao Huai-Rong Shen Yuan Li |
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