NCADE导弹建模与仿真研究
Research on Modeling and Simulation of NCADE Missile
Received date: 2013-03-26
Online published: 2025-05-26
袁宴波 , 雷科 . NCADE导弹建模与仿真研究[J]. 弹箭与制导学报, 2013 , 33(6) : 6 -8 . DOI: 10.15892/j.cnki.djzdxb.2013.06.018
The NCADE is an airborne antimissile missile developed by Raytheon company in the US. In order to obtain the exact trajectory character of NCADE, a mathematical model is established and a reasonable guidance and control algorism is designed based on the character of the missile, the digital simulation of the NCADE missile is carried out subsequently. Simulation result shows that the key factor of NCADE missile's ability to hit the target directly is achieved by its adoption of an orbit control mode reaction-jet control system which is essential to accomplish kinetic energy interception against high speed ballistic missiles.
Key words: NCADE missile; reaction-jet control; missile modeling; digital simulation
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