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Key Techniques of Terminal Correction Mortar Projectiles 被引量:2

Key Techniques of Terminal Correction Mortar Projectiles
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摘要 The operational principle, the impulse force and terminal guidance laws of terminal correction mortar projectiles(TCMP) are researched in this paper, by using the TCMP simulation program, key techniques such as the miss distance influenced by the acting point of impulse force, the impulse force value, the correction threshold, and the number of impulse rockets are researched in this paper. And the dual pulse control scheme is also studied. Simulation results indicate that the best acting point is near the center of gravity, sufficient correction resources are needed, the miss distance is insentive to the correction threshold, increasing the number of impulse rockets properly is beneficial to increase the hit precision, the velocity pursuit guidance law has less miss distance, the change of the attack angle is milder and the transient time becomes less in the dual impulse control scheme. These conclusions are important for choosing parameters and impulse correction schemes designed for TCMP. The operational principle, the impulse force and terminal guidance laws of terminal correction mortar projectiles(TCMP) are researched in this paper, by using the TCMP simulation program, key techniques such as the miss distance influenced by the acting point of impulse force, the impulse force value, the correction threshold, and the number of impulse rockets are researched in this paper. And the dual pulse control scheme is also studied. Simulation results indicate that the best acting point is near the center of gravity, sufficient correction resources are needed, the miss distance is insentive to the correction threshold, increasing the number of impulse rockets properly is beneficial to increase the hit precision, the velocity pursuit guidance law has less miss distance, the change of the attack angle is milder and the transient time becomes less in the dual impulse control scheme. These conclusions are important for choosing parameters and impulse correction schemes designed for TCMP.
作者 徐劲祥
出处 《Journal of Beijing Institute of Technology》 EI CAS 2007年第2期168-172,共5页 北京理工大学学报(英文版)
基金 Sponsored by the Ministerial Level Advanced Research Foundation (40406030101)
关键词 terminal correction mortar projectile (TCMP) tracking error angle correction threshold dualpulse control miss distance terminal correction mortar projectile (TCMP) tracking error angle correction threshold dualpulse control miss distance
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  • 1肖先国,万春熙.中间段制导兵器的原理和技术途径的研究[J].兵工学报(弹箭分册),1989(3):27-34. 被引量:3
  • 2邓大新.简易制导技术在舰载火箭弹中应用 [D].武汉:海军工程大学,1999.
  • 3徐明友.火箭外弹道学 [M].北京:兵器工业出版社,1998.
  • 4Joe B. Low cost course correctien (LCCC) for the M261 Hydra-70 Rocket[A]. 2002 Missiles and Rockets Symposium[C]. Panama: General Dynamics, 2002.1- 17
  • 5徐劲祥.[D].北京:北京理工大学,2004.
  • 6谭凤岗.弹道修正弹的概念研究[J].弹箭技术,1998,9(4):1-10. 被引量:47

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