Bezier-curve Navigation Guidance for Impact Time and Angle Control
This paper addresses a novel impact time and angle control guidance law using a Bézier curve. The 2nd order Bézier curve consists of one control point and two boundary points; initial point P0, middle point P1 and end point P2. The curve is tangent to the line P0-P1 and the line P1-P2, respectively,...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2018-03-01
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| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/moon_shim_tahk_vol_10_iss_1.pdf |
| _version_ | 1818162198059417600 |
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| author | Gun-Hee MOON Sang-Wook SHIM Min-Jea TAHK |
| author_facet | Gun-Hee MOON Sang-Wook SHIM Min-Jea TAHK |
| author_sort | Gun-Hee MOON |
| collection | DOAJ |
| description | This paper addresses a novel impact time and angle control guidance law using a Bézier curve. The 2nd order Bézier curve consists of one control point and two boundary points; initial point P0, middle point P1 and end point P2. The curve is tangent to the line P0-P1 and the line P1-P2, respectively, and always exists in the convex hull of the control points. Proposed Bézier curve navigation guidance, makes the missile follow the Bézier curve with the feedback form of guidance command so that the missile hits the target on the desired time in the desired direction. We conducted numerical simulations on several terminal conditions to demonstrate the performance of proposed method. |
| first_indexed | 2024-12-11T16:29:51Z |
| format | Article |
| id | doaj.art-3b8ec9c451c74421b62c0c6498f8650f |
| institution | Directory Open Access Journal |
| issn | 2066-8201 2247-4528 |
| language | English |
| last_indexed | 2024-12-11T16:29:51Z |
| publishDate | 2018-03-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| series | INCAS Bulletin |
| spelling | doaj.art-3b8ec9c451c74421b62c0c6498f8650f2022-12-22T00:58:37ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282018-03-0110110511510.13111/2066-8201.2018.10.1.11Bezier-curve Navigation Guidance for Impact Time and Angle ControlGun-Hee MOON0Sang-Wook SHIM1Min-Jea TAHK2Korea Advanced Institute of Science and Technology, Daehakro 291 KAIST, Yeuseunggu, Daejeon, Republic of Korea, ghmoon@fdcl.kaist.ac.krKorea Advanced Institute of Science and Technology, Daehakro 291 KAIST, Yeuseunggu, Daejeon, Republic of Korea, swshim@fdcl.kaist.ac.krKorea Advanced Institute of Science and Technology, Daehakro 291 KAIST, Yeuseunggu, Daejeon, Republic of Korea, mjtahk317@gmail.com*This paper addresses a novel impact time and angle control guidance law using a Bézier curve. The 2nd order Bézier curve consists of one control point and two boundary points; initial point P0, middle point P1 and end point P2. The curve is tangent to the line P0-P1 and the line P1-P2, respectively, and always exists in the convex hull of the control points. Proposed Bézier curve navigation guidance, makes the missile follow the Bézier curve with the feedback form of guidance command so that the missile hits the target on the desired time in the desired direction. We conducted numerical simulations on several terminal conditions to demonstrate the performance of proposed method.http://bulletin.incas.ro/files/moon_shim_tahk_vol_10_iss_1.pdfBézier-curve navigation guidanceimpact timeimpact angleanti-ship missiles |
| spellingShingle | Gun-Hee MOON Sang-Wook SHIM Min-Jea TAHK Bezier-curve Navigation Guidance for Impact Time and Angle Control INCAS Bulletin Bézier-curve navigation guidance impact time impact angle anti-ship missiles |
| title | Bezier-curve Navigation Guidance for Impact Time and Angle Control |
| title_full | Bezier-curve Navigation Guidance for Impact Time and Angle Control |
| title_fullStr | Bezier-curve Navigation Guidance for Impact Time and Angle Control |
| title_full_unstemmed | Bezier-curve Navigation Guidance for Impact Time and Angle Control |
| title_short | Bezier-curve Navigation Guidance for Impact Time and Angle Control |
| title_sort | bezier curve navigation guidance for impact time and angle control |
| topic | Bézier-curve navigation guidance impact time impact angle anti-ship missiles |
| url | http://bulletin.incas.ro/files/moon_shim_tahk_vol_10_iss_1.pdf |
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