Ideal trajectory generation method of missile formation based on Gaussian pseudo-spectrum method Article Swipe
YOU?
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· 2023
· Open Access
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· DOI: https://doi.org/10.1088/1742-6596/2478/10/102005
With the increasingly complex combat environment and the diversity of combat tasks, important military targets are surrounded by multi-layer defense. Modern information warfare pays more attention to system confrontation and multi-system cooperative operations,and missile formation to attack targets is the main research content of this paper. For missile wing ideal trajectory generation problems, ensure the attack Angle of time and meet the design requirements, Gaussian pseudo-spectral method is used to generate guarantee missile attacks within the specified time shot on target, at the same time meet the attack Angle constraint at the end of the ideal trajectory, the more missiles cooperative engagement problems into the ideal trajectory tracking problem, avoid the estimate of the remaining time of flight.The main contents of this paper are as follows:(1) Gaussian pseudo-spectral method is used to generate the ideal trajectory model.(2)Use Matlab to simulate the established model.
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- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.1088/1742-6596/2478/10/102005
- https://iopscience.iop.org/article/10.1088/1742-6596/2478/10/102005/pdf
- OA Status
- diamond
- References
- 4
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W4381996890
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W4381996890Canonical identifier for this work in OpenAlex
- DOI
-
https://doi.org/10.1088/1742-6596/2478/10/102005Digital Object Identifier
- Title
-
Ideal trajectory generation method of missile formation based on Gaussian pseudo-spectrum methodWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2023Year of publication
- Publication date
-
2023-06-01Full publication date if available
- Authors
-
Benkang Zhang, Jian Shen, Xiaoguang Wang, Qingyu ZhuList of authors in order
- Landing page
-
https://doi.org/10.1088/1742-6596/2478/10/102005Publisher landing page
- PDF URL
-
https://iopscience.iop.org/article/10.1088/1742-6596/2478/10/102005/pdfDirect link to full text PDF
- Open access
-
YesWhether a free full text is available
- OA status
-
diamondOpen access status per OpenAlex
- OA URL
-
https://iopscience.iop.org/article/10.1088/1742-6596/2478/10/102005/pdfDirect OA link when available
- Concepts
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Missile, Trajectory, Ideal (ethics), Missile guidance, MATLAB, Computer science, Gaussian, Missile defense, Constraint (computer-aided design), Control theory (sociology), Mathematical optimization, Engineering, Aerospace engineering, Artificial intelligence, Mathematics, Law, Physics, Quantum mechanics, Mechanical engineering, Operating system, Control (management), Astronomy, Political scienceTop concepts (fields/topics) attached by OpenAlex
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0Total citation count in OpenAlex
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4Number of works referenced by this work
- Related works (count)
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10Other works algorithmically related by OpenAlex
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| primary_location.is_accepted | True |
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| primary_location.raw_source_name | Journal of Physics: Conference Series |
| primary_location.landing_page_url | https://doi.org/10.1088/1742-6596/2478/10/102005 |
| publication_date | 2023-06-01 |
| publication_year | 2023 |
| referenced_works | https://openalex.org/W4298060601, https://openalex.org/W1980693151, https://openalex.org/W2138313151, https://openalex.org/W2126441924 |
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