Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space
Cooperative guidance problem of multiple missile system in three-dimensional space is investigated in this paper. Guidance commands in pitch plane and lateral plane of initial guidance, mid-course guidance and terminal guidance are designed, and the rules of shift guidance in different guidance stag...
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Editorial Office of Aero Weaponry
2021
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oai:doaj.org-article:08adb432e4724d62b074de30dd5fce542021-11-30T00:13:56ZCompound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space1673-504810.12132/ISSN.1673-5048.2019.0168https://doaj.org/article/08adb432e4724d62b074de30dd5fce542021-02-01T00:00:00Zhttp://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/1616466613419-1435279413.pdfhttps://doaj.org/toc/1673-5048Cooperative guidance problem of multiple missile system in three-dimensional space is investigated in this paper. Guidance commands in pitch plane and lateral plane of initial guidance, mid-course guidance and terminal guidance are designed, and the rules of shift guidance in different guidance stages are given.The numerical simulation results of high parabolic trajectory are given in two cases, and the performance characteristics of the compound cooperative guidance law are obtained. The effectiveness of the theoretical method proposed in this paper is verified, which provides a possible solution to the problem of multi-missile cooperative attack.Zhao Qilun,Song Xun,Wang Xiaodong,Wang MengyiEditorial Office of Aero Weaponryarticle|missile guidance|high parabolic trajectory|cooperative guidance|impact time constraint|compound guidanceMotor vehicles. Aeronautics. AstronauticsTL1-4050ZHHangkong bingqi, Vol 28, Iss 1, Pp 26-33 (2021) |
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|missile guidance|high parabolic trajectory|cooperative guidance|impact time constraint|compound guidance Motor vehicles. Aeronautics. Astronautics TL1-4050 |
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|missile guidance|high parabolic trajectory|cooperative guidance|impact time constraint|compound guidance Motor vehicles. Aeronautics. Astronautics TL1-4050 Zhao Qilun,Song Xun,Wang Xiaodong,Wang Mengyi Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space |
description |
Cooperative guidance problem of multiple missile system in three-dimensional space is investigated in this paper. Guidance commands in pitch plane and lateral plane of initial guidance, mid-course guidance and terminal guidance are designed, and the rules of shift guidance in different guidance stages are given.The numerical simulation results of high parabolic trajectory are given in two cases, and the performance characteristics of the compound cooperative guidance law are obtained. The effectiveness of the theoretical method proposed in this paper is verified, which provides a possible solution to the problem of multi-missile cooperative attack. |
format |
article |
author |
Zhao Qilun,Song Xun,Wang Xiaodong,Wang Mengyi |
author_facet |
Zhao Qilun,Song Xun,Wang Xiaodong,Wang Mengyi |
author_sort |
Zhao Qilun,Song Xun,Wang Xiaodong,Wang Mengyi |
title |
Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space |
title_short |
Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space |
title_full |
Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space |
title_fullStr |
Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space |
title_full_unstemmed |
Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space |
title_sort |
compound cooperative guidance for high parabolic trajectory in three-dimensional space |
publisher |
Editorial Office of Aero Weaponry |
publishDate |
2021 |
url |
https://doaj.org/article/08adb432e4724d62b074de30dd5fce54 |
work_keys_str_mv |
AT zhaoqilunsongxunwangxiaodongwangmengyi compoundcooperativeguidanceforhighparabolictrajectoryinthreedimensionalspace |
_version_ |
1718406843505573888 |