Compensation analysis of subsidence angle of supersonic low-altitude cruise target projectile launch

Aiming at the launching process of the supersonic barrel-type spinning target projectile, and improving the control accuracy of the open-loop controlled target projectile, making the subsidence angle compensation can improve the accuracy of the launching process, and make the actual flight trajector...

Full description

Saved in:
Bibliographic Details
Published in:Journal of physics. Conference series Vol. 2336; no. 1; pp. 12011 - 12017
Main Authors: Guo, Hongli, Ren, Shaofeng, Yan, Huaiqiang, Zhao, Hongtao, Wei, Chunshuang, Gao, Yun
Format: Journal Article
Language:English
Published: Bristol IOP Publishing 01.08.2022
Subjects:
Accuracy
Barrel launch
Compensation
Flight trajectory
Low altitude
Physics
Projectiles
Spin target projectile
Subsidence
Subsidence angle
Trajectory control
ISSN:1742-6588, 1742-6596
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:Aiming at the launching process of the supersonic barrel-type spinning target projectile, and improving the control accuracy of the open-loop controlled target projectile, making the subsidence angle compensation can improve the accuracy of the launching process, and make the actual flight trajectory closer to the preset theoretical simulation trajectory. Studies have shown that the subsidence angle of the initial launch has a great impact on the actual flight trajectory. To achieve the same control effect, it must be adjusted to the corresponding control strategy. In this article, we provided the subsidence angle analysis method, which can truly reflect the change of the subsidence angle, and realize the precise control of the trajectory through effective compensation. CCS Concepts: Computing methodologies~Modeling and simulation~Model development and analysis~Model verification and validation
Bibliography:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:1742-6588
1742-6596
DOI:10.1088/1742-6596/2336/1/012011