Time-Delay Control for Integrated Missile Guidance and Control
In this paper, integrated missile guidance and control systems using time-delay control (TDC) are developed. The next generation missile requires that an interceptor hits the target, maneuvering with small miss-distances, and has lower weight to reduce costs. This is possible if the synergism existi...
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| Vydané v: | International journal of aeronautical and space sciences Ročník 12; číslo 3; s. 260 - 265 |
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| Hlavní autori: | , , |
| Médium: | Journal Article |
| Jazyk: | English |
| Vydavateľské údaje: |
한국항공우주학회
2011
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| Predmet: | |
| ISSN: | 2093-274X, 2093-2480 |
| On-line prístup: | Získať plný text |
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| Shrnutí: | In this paper, integrated missile guidance and control systems using time-delay control (TDC) are developed. The next generation missile requires that an interceptor hits the target, maneuvering with small miss-distances, and has lower weight to reduce costs. This is possible if the synergism existing between the guidance and control subsystems is exploited by the integrated controller. The TDC law is a robust control technique for nonlinear systems, and it has a very simple structure. The feature of TDC is to directly estimate the unknown dynamics and the unexpected disturbance using one-step time-delay. To investigate the performance of the integrated controller, numerical simulations are performed as the maneuver of the target. The results show that the integrated guidance and control system has a good performance. KCI Citation Count: 2 |
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| Bibliografia: | G704-SER000009560.2011.12.3.002 |
| ISSN: | 2093-274X 2093-2480 |
| DOI: | 10.5139/IJASS.2011.12.3.260 |