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智能蒙皮飞行器的飞行控制研究 被引量:10

Research on Flight Control of a Smart Skin Aircraft
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摘要 将嵌入大量微致动器元件的智能蒙皮应用于飞行器,以增强或替代传统的控制面来产生控制力矩,使飞行器稳定并能进行机动飞行。以无尾飞行器为例,推导了其动力学模型,并设计了状态反馈控制器。仿真结果表明,所讨论的智能蒙皮对机动要求不大的无尾飞行器具有足够的控制能力。 The smart skin which embedded hundreds of micro effectors was used in an advanced aircraft to generate moments for stabilization and maneuver, by augmenting or replacing conventional control surfaces. In this paper a tailless aircraft was used as a model. Its dynamics was derived and the state-feedback controller was designed. The dynamic simulation results indicate that the smart skin studied in the paper is able to maintain a sufficient authority to control the tailless aircraft in a low-rate maneuvering.
作者 杨士斌 徐敏
出处 《飞行力学》 CSCD 北大核心 2007年第1期39-42,共4页 Flight Dynamics
基金 国家自然科学基金重大研究计划资助项目(90405002)
关键词 智能蒙皮 微致动器阵列 无尾飞行器 smart skin micro effector arrays tailless aircraft
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参考文献4

  • 1David Raney, Raymond Montgomery, Larwence Green.Flight Control Using Distributed Shape-Change Effector Arrays[ R]. AIAA 2000-1560,2000.
  • 2Kenneth Bordignon, Wayne Durham. Closed-Form Solutions to Constrained Control Allocation Problem[ J ]. Journal of Guidance, Control, and Dynamics, 1995,18 (5) :1 000-1 007.
  • 3Ralph Paul, William Garrard. Dynamics and Control of Tailless Aircraft[ R]. AIAA 97-3776,1997.
  • 4Franklin, Powell, Naeini. Feedback Control of Dynamic Systems [ M ]. Addison-Wesley Publishing Company,1986.

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