Dynamics of a deflectable-nose missile

Author:

Sun XiaoFeng,Gu LiangXian,Gong ChunLin

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference21 articles.

1. Nielsen J N. Missile Aerodynamics. New York: McGraw Hill, 1960

2. Landers M G, Auman L M. Experimental investigation of nose-mounted controls for a hypersonic missile. In: Proceedings of the 2001 AIAA 19th Applied Aerodynamics Conference. Anaheim: AIAA, 2001.2433

3. Chen P C, Sulaeman E, Liu D D, et al. Body-flexure control with smart actuation for hypervelocity missiles. In: Proceedings of the 2003 AIAA 44th Structures, Structural Dynamics, and Materials Conference. Norfolk: AIAA, 2003. 1965

4. Yang C, Song C, Wu Z G, et al. Application of output feedback sliding model to active flutter suppression of two-dimensional airfoil. Sci China Tech Sci, 2010, 53: 1338–1348

5. Cao D Q, Zhao N. Active control of supersonic/hypersonic aeroelastic flutter for a two-dimensional airfoil with flap. Sci China Tech Sci, 2011, 54: 1943–1953

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