Motion Coupling Analysis for the Nose and Body of the Deflectable Nose Missile

Article Preview

Abstract:

The chief aim of the present study is to find the effect of the nose motion upon the main body of the deflectable nose missile. The dynamic model including the motions of the nose and main body is built. The dynamic simulation and analysis show the interferential moment of the nose and main body can cause disadvantageous “body flutter”. The coupling motions can be decreased through lightening the weight of the nose. The coupling motion can be decreased greatly when the point of hinge、mass center the nose are set on one place. The roll increases the motion coupling of the three channels of the missile.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

260-263

Citation:

Online since:

July 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2011 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Landers M G, Dynetics L H, Auman L M, Jr M E. Deflectable Nose and Canard Control for Fin Stabilized Projectile at Supersonic and Hypersonic Speeds. AIAA-3805(2003).

DOI: 10.2514/6.2003-3805

Google Scholar

[2] Milton E, Jr M E, Auman L M. a Productivity-Oriented Application of Computational Fluid Dynamics to the Design of a Hypervelocity Missile. AIAA-2937(2002).

DOI: 10.2514/6.2002-2937

Google Scholar

[3] Vaughn M E, Jr M E, Auman L M. Assessment of a Productivity-Oriented CFD Methodology for Designing a Hypervelocity Missile. AIAA-3937(2002).

DOI: 10.2514/6.2003-3937

Google Scholar

[4] Barrett R M, Brozoski F, Gross R S. Design and Testing of a Subsonic All-Moving Adaptive Flight Control Surface. AIAA Journal, VOL. 35 (1997), pp.1217-1219.

DOI: 10.2514/3.13649

Google Scholar

[5] Wang Xugang, Zhou Jun. Dynamic and mathematical Model of the Deflectable Nose Missile. Journal of Northwestern Polytechnical University, VOL. 25 (2007), pp.556-560.

Google Scholar

[6] Qian Xingfang, Lin Ruixiong, Zhao Yanan. Dynamics of the Flight for the Missile. ( Publishing House of Beijing Institute of Technology, Beijing, 2000).

Google Scholar