Journal of Projectiles, Rockets, Missiles and Guidance >
Motion Analysis on Mass Servo System of Moving Mass Interception Missiles
Received date: 2014-05-19
Online published: 2025-05-26
The's mass-center changes with mass motion, and then the attitude angles change, thereby; the missile could be controlled to attack target. A coupled nonlinear system equations proposed based on the characteristics of the dynamics, with the analysis of the mass servo system, inertia moment and the coupling of the states researched. A series of simulation aboutmissile attitude performed so as to lay a foundation developing the control mechanism and application of the missiles.
Key words： moving mass; mass servo system; motion analysis
YAO Chunming , LI Xiaobing , WU Bowen , BAI Ruiyang . Motion Analysis on Mass Servo System of Moving Mass Interception Missiles[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(3) : 47 -49,92 . DOI: 10.15892/j.cnki.djzdxb.2015.03.013
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