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Synthesis of Guidance Law for Air-To-Air Missile Intercepts Separating Targets at Long Distances

Tuan, N.T. and Tien, V.H. and Minh, D.V. and Hung, N.N. (2023) Synthesis of Guidance Law for Air-To-Air Missile Intercepts Separating Targets at Long Distances. Journal of Aeronautics, Astronautics and Aviation, 55 (4). pp. 507-515.

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Abstract

This paper presents the results synthesis of an optimal guidance law for air-to-air missiles (AAM) to intercept separating targets at a long distance. Based on the optimal filtering theory, this proposed guidance law allows interceptor missiles to distinguish each target in a group according to the Doppler frequency of each target and guides the missile to a selected target in the group. The simulation results have proved that the proposed guidance law is highly effective when intercepting a separating target, one of the particularly dangerous types of targets. © 2023 The Aeronautical and Astronautical Society of the Republic of China. All rights reserved.

Item Type: Article
Divisions: Offices > Office of International Cooperation
Identification Number: 10.6125/JoAAA.20231255(4).01
Uncontrolled Keywords: Electronic guidance systems; Guided missiles, Air-to-air missiles; Guidance laws; Long-range air-to-air missile; Maneuverable targets; Navigation law; Optimal filtering theory; Optimal guidance law; Optimal proportional preemptive navigation law; Separating target; Super maneuverable target, Air navigation
Additional Information: cited By 0
URI: http://eprints.lqdtu.edu.vn/id/eprint/11018

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