DC Field | Value | Language |
---|---|---|
dc.contributor.author | Tahk, Min-Jea | ko |
dc.contributor.author | Park, Jong-Chan | ko |
dc.contributor.author | Rho, Heekun | ko |
dc.contributor.author | Lee, Chang-Hun | ko |
dc.date.accessioned | 2023-11-20T08:02:15Z | - |
dc.date.available | 2023-11-20T08:02:15Z | - |
dc.date.created | 2023-11-20 | - |
dc.date.issued | 2023-07-20 | - |
dc.identifier.citation | 2023 14th International Conference on Mechanical and Aerospace Engineering | - |
dc.identifier.uri | http://hdl.handle.net/10203/314876 | - |
dc.description.abstract | A numerically efficient method is proposed to produce high-performance suboptimal trajectories for maximizing terminal speed in long-range air-to-air missile engagements. Pursuit guidance is augmented by a linear lead-angle bias function and combined with homing guidance such as proportional navigation and impact-angle-control guidance to quickly generate a suboptimal trajectory very close to the optimal trajectory while satisfying terminal constraints. Numerical results for various engagement scenarios are provided to demonstrate the usefulness of the proposed method for real-time optimal midcourse guidance. | - |
dc.language | English | - |
dc.publisher | IEEE, Science and Engineering Institute | - |
dc.title | Suboptimal Guidance Based on Pursuit and Impact Angle Control for Long-Range Air-to-Air Missiles | - |
dc.type | Conference | - |
dc.type.rims | CONF | - |
dc.citation.publicationname | 2023 14th International Conference on Mechanical and Aerospace Engineering | - |
dc.identifier.conferencecountry | PO | - |
dc.identifier.conferencelocation | Porto | - |
dc.contributor.localauthor | Tahk, Min-Jea | - |
dc.contributor.localauthor | Lee, Chang-Hun | - |
dc.contributor.nonIdAuthor | Rho, Heekun | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.