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
Hlavní autori: Park, Bong-Gyun, Kim, Tae-Hun, Tahk, Min-Jea
Médium: Journal Article
Jazyk:English
Vydavateľské údaje: 한국항공우주학회 2011
Predmet:
항공우주공학
Zero-effort miss
Autopilot
Time-delay control
Integrated guidance and control
Guidance law
ISSN:2093-274X, 2093-2480
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Abstract 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
AbstractList 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
Author Min-Jea Tahk
Tae-Hun Kim
Bong-Gyun Park
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Keywords Zero-effort miss
Autopilot
Time-delay control
Integrated guidance and control
Guidance law
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Title Time-Delay Control for Integrated Missile Guidance and Control
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