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http://dx.doi.org/10.5139/JKSAS.2022.50.6.393

High-Altitude Terminal Guidance and Control Loop Design Using Thrust Vector Control  

Jeon, Ha-Min (Department of Aerospace Engineering, Inha University)
Park, Jongho (Department of Military Digital Convergence, Ajou University)
Ryoo, Chang-Kyung (Department of Aerospace Engineering, Inha University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.50, no.6, 2022 , pp. 393-400 More about this Journal
Abstract
The Divert and Attitude Control System(DACS) used in high-altitude engagements is expensive and complex. In this paper, we design a high-altitude terminal guidance and control loop of guided-missile equipped with a Thrust Vector Control(TVC) that is less expensive and simpler than DACS. The proposed system utilizes a quaternion feedback control technique to track the thrust attitude command converted from the acceleration command of true proportional navigation guidance. The performance analysis of the proposed terminal guidance and control loop is conducted through engagement simulations against ballistic targets at a high altitude.
Keywords
Thrust Vector Control; Thrust Attitude Command; Quaternion Feedback Control; Terminal Boosting;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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