@inproceedings{51c841a4ab614086a3a740f09fd5e723,
title = "Modeling and simulation research of missile with deflectable nose",
abstract = "With respect to a kind of missile with deflectable nose, six-degree-of-freedom dynamics mathematical model including deflectable nose dynamic was established using momentum principle, and guidance system model was presented, at the same time the whole attitude control system with deflectable nose was designed based on variable structure control theory. In order to prove the correctness of the validity of the altitude control strategy, under the environment of MATLAB6.5/SIMULINK, the six-degree-of-freedom digital simulation system was studied and developed for missile with deflectable nose. Finally simulation about non-maneuverable target and the snake-shape maneuverable target were conducted; the results validate the strong maneuverability and intercepting capability of the supersonic missile with deflectable nose, and show the designed control method was effective to the attitude control system.",
keywords = "Deflectable nose, Model, Nonlinear, Simulation, Variable structure control",
author = "Guo, {Jian Guo} and He, {Yuan Jun} and Jun Zhou",
year = "2009",
doi = "10.1109/ICICISYS.2009.5358134",
language = "英语",
isbn = "9781424447541",
series = "Proceedings - 2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009",
pages = "86--89",
booktitle = "Proceedings - 2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009",
note = "2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009 ; Conference date: 20-11-2009 Through 22-11-2009",
}