• Infrared and Laser Engineering
  • Vol. 51, Issue 7, 20210558 (2022)
Musheng Luo1, Fengquan Yu1, Junmin Wang2, and Mansi Li2
Author Affiliations
  • 1Naval Aviation University, Yantai 264001, China
  • 2Unit 91001 of PLA, Beijing 100841, China
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    DOI: 10.3788/IRLA20210558 Cite this Article
    Musheng Luo, Fengquan Yu, Junmin Wang, Mansi Li. Analytical calculation method of the maximum attack angle of an infrared guided air-to-ship missile[J]. Infrared and Laser Engineering, 2022, 51(7): 20210558 Copy Citation Text show less

    Abstract

    Aiming at the angle of attack, which is an important influencing factor of infrared guided air-to-ship missile path planning, constraint models of the attack angle were built, including the number of waypoints, distance between two adjacent waypoints, turning angle and pathway distance. An analytical calculation method of the maximum attack angle was proposed. Applying the principle of geometry, the maximum angle of attack calculation model was built, which could be used to solve the pathway with one waypoint, two waypoints and multiple points. Finally, the maximum attack angle under different conditions was simulated when the waypoint number, turning angle and missile range were changed separately. The results show that the maximum angle of attack would increase rapidly as the missile path waypoint increased; it would also increase as the turning angle decreased if the waypoint number was constant. However, the attack angle increased at the expense of the infrared guided air-to-ship missile range.
    Musheng Luo, Fengquan Yu, Junmin Wang, Mansi Li. Analytical calculation method of the maximum attack angle of an infrared guided air-to-ship missile[J]. Infrared and Laser Engineering, 2022, 51(7): 20210558
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