Research on the navigation method of large-scale differential tail-control improvised guided munitions based on rotational speed constraints

In the process of launching guided projectile under the conventional system, it is difficult to effectively obtain the precise navigation parameters of the projectile in the high dynamic environment. Aiming at this problem, this paper describes a new system of guided ammunition based on tail spin re...

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Veröffentlicht in:	Defence technology Jg. 38; H. 8; S. 155 - 170
Hauptverfasser:	Liu, Ning, Zhao, Wenjiang, Wang, Yao, Shen, Kai, Su, Zhong, Qi, Wenhao, Xie, Yuedong
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Beijing Elsevier B.V 01.08.2024 KeAi Publishing Communications Ltd Beijing Key Laboratory of High Dynamic Navigation Technology,Beijing Information Science and Technology University,Beijing,100192,China%Hua an Industry Group Co.,Ltd.,Qiqihar,161006,China%Integrated Navigation and Intelligent Navigation Laboratory,Beijing Institute of Technology,Beijing,100081,China%Beijing Institute of Technology,Beijing,100081,China KeAi Communications Co., Ltd
Schlagworte:	Accuracy Algorithms Ammunition Combined navigation Constraints Control systems Extended Kalman filter Extended Kalman filter (EKF) Flight tests Guided projectiles Hardware-in-the-loop simulation High speed Kalman filters Launching Military supplies Military technology Missile control Navigation Navigation systems Neural networks Parameter estimation Process parameters Projectiles RPM constraints Simulation Spin dynamics Spin reduction Tail spin reduction Velocity Velocity errors Tail spin reduction Extended Kalman filter (EKF) Guided projectiles RPM constraints Combined navigation Extended Kalman filter(EKF)
ISSN:	2214-9147, 2096-3459, 2214-9147
Online-Zugang:	Volltext
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