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Time-Delay Control for Integrated Missile Guidance and Control
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 Title & Authors
Time-Delay Control for Integrated Missile Guidance and Control
Park, Bong-Gyun; Kim, Tae-Hun; Tahk, Min-Jea;
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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.
 Keywords
Time-delay control;Autopilot;Guidance law;Integrated guidance and control;Zero-effort miss;
 Language
English
 Cited by
1.
Adaptive Integrated Guidance and Control Design for a Missile With Input Constraints, IFAC Proceedings Volumes, 2013, 46, 20, 206  crossref(new windwow)
2.
Full-State Autopilot-Guidance Design Under a Linear Quadratic Differential Game Formulation, IFAC Proceedings Volumes, 2014, 47, 3, 3942  crossref(new windwow)
3.
Linear Quadratic Integrated Versus Separated Autopilot-Guidance Design, Journal of Guidance, Control, and Dynamics, 2013, 36, 6, 1722  crossref(new windwow)
4.
Single Versus Two-Loop Full-State Multi-Input Missile Guidance, Journal of Guidance, Control, and Dynamics, 2015, 38, 5, 843  crossref(new windwow)
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