期刊文献+

可变形翼战术导弹的研究与发展 被引量:8

Research and Development of Tactical Missile with Morphing Wing
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摘要 介绍了变形翼技术的应用概况,重点阐述了其在战术导弹上的研究现状,分析了可变形翼战术导弹所具有的若干技术优势,总结出涉及可变形翼战术导弹研究的几项关键技术,指出其研究与发展的新趋势。
出处 《航空科学技术》 2011年第1期18-21,共4页 Aeronautical Science & Technology
基金 航空科学基金(2008ZA12001)资助
关键词 可变形翼 战术导弹 多操纵面 智能材料 morphing wing tactical missile multiple control effectors intelligent material
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参考文献14

  • 1Armando R. Rodriguez Morphing Aircraft Technology Survey[R] AIAA 2007- 1258, 2007.
  • 2Terrence A. Weisshaar. Morphing Aircraft Technology-New Shapes for Aircraft Design[R]. NATO - RTO - MP - AVT- 141, 2006.
  • 3Michael I. Friswell, Daniel J. Inman. Concepts for UAVs[C]. 21st Bristol UAV Systems Conference, April 2006.
  • 4Derek R. Bye, Paul D. McClure. Design of a Morphing Vehicle[R]. AIAA - 2007 - 1728, 2007.
  • 5Jouannet C., Lundstrom D., Amadori K., et al. Morphing Wing Design, from Study to Flight Test[R]. AIAA- 2009 - 1619, 2009.
  • 6Anna Maria R. McGowan, Martin R. Waszak. NASA's Morphing Project Research Summaries .in Fiscal Year 2002[R]. NASA/TM - 2005 - 213266, 2005.
  • 7Sahjendra N. Singh, Marc Steinberg, Robert D. Digirolamo. Variable Structures Robust Flight Control Systems for the F-14[J]. IEEE Trans. On Aerospace and Electronic Systems,1997, 33 (1): 77-84.
  • 8Gary J. Balas, Andrew K. Packard., Joe Renfrow, et al. Control of the F 14 Aircraft Lateral Directional Axis During Powered Approach[J]. Journal of Guidance, Control and Dynamics, 21 (6): 899- 908, 1998.
  • 9Painter W.D., AD 1 Oblique Wing Research Aircraft Pilot Evaluation Program[R]. AIAA- 83 - 2509, 1983.
  • 10Michael J. Hirschberg, David M. Hart, Thomas J. Beutner. A Summary of A Half- Century of Oblique Wing Research[R]. http://www.desktopaero. com/, June 2005.

二级参考文献6

  • 1D A Neal, M G Good. Design and wind - tunnel analysis of a fully adaptive aircraft configuration[ C]. AIAA2004 -1727.
  • 2P Marmier, N M Wereley. Morphing wings of a small scale UAV using inflatable actuators Sweep control[ C ]. AIAA2003 - 1802.
  • 3J M Lafeur, J R Olders, R Braun. Daedalon:A Revolutionary Morphing Spacecraft Design for Planetary Exploration[ C]. AIAA2005 - 2771.
  • 4T T Takahashi, R J Spall, D C Turner, M Bimey. A Multi -Disciplinary Survey of Advanced Subsonic Tactical Cruise Missile Configurations[ C ]. AIAA 2005 - 0709.
  • 5J Y Hung, W B Gao, J C Hung. Variable Structure Control: A Survey[J]. IEEE Trans. Industrial Electronics, 1993, 40(1).
  • 6Andrzej. An Inverse Simulation Study on Wing Adapter Kit Dynamics and Control in Prescribed Trajectory Flight [ C ]. AIAA 2006 - 829.

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同被引文献52

引证文献8

二级引证文献34

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