EVALUATING EFFECTIVENESS OF EXTENDING ENGAGEMENT ZONE OF SURFACE-TO-AIR MISSILE USING THE COMBINATIONAL GUIDANCE LAW CV-2DGOC

Authors

  • Thanh Tung Nguyen Le Quy Don Technical University
  • Cong Dinh Nguyen Le Quy Don Technical University
  • Hoa Tien Vu Le Quy Don Technical University
  • Quang Anh Nguyen Le Quy Don Technical University

DOI:

https://doi.org/10.56651/lqdtu.jst.v14.n01.497

Keywords:

Guidance law; combinational guidance law; engagement zone; surface-to-air missile.

Abstract

The combinational guidance law (denoted CV-2DGOC) created by the combination of the rainbow guidance law and the two-point guidance law considering impact angle proved important specified requirement of guidance accuracy due to maintaining missile kinetic energy or missile speed to produce commanded lateral acceleration. In this paper, the authors show capability of extending the engagement zone because of optimizing trajectory both powered flight phase and unpowered flight phase. Boundaries of engagement zone are determined based on analyzing dynamic of missile guidance closed-loop using traditional lead half angle guidance law and combinational guidance law (CV-2DGOC) in same engagement scenarios. Simulation has been conducted to validate effectiveness of expanding size of engagement zone.

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Published

2022-10-28

How to Cite

Nguyen, T. T. ., Nguyen, C. D. ., Vu, H. T. ., & Nguyen, Q. A. . (2022). EVALUATING EFFECTIVENESS OF EXTENDING ENGAGEMENT ZONE OF SURFACE-TO-AIR MISSILE USING THE COMBINATIONAL GUIDANCE LAW CV-2DGOC. Journal of Science and Technique, 14(01). https://doi.org/10.56651/lqdtu.jst.v14.n01.497

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