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飞行控制与飞机发展 被引量:18

Development of flight control with aircraft
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摘要 论述飞行控制技术的发展及其与飞机发展的关系 .概要回顾了自莱特兄弟研究人类飞行技术开始至 2 0世纪 60年代初期飞机飞行控制技术的发展过程 .阐述了主动控制技术与电传飞行控制系统的产生和对飞机发展的巨大影响 . The flight control technology development and effects on aircraft were discussed. It was briefly reviewed that history from Wright brothers to 1960s'. The emergence of active control technology and fly-by-wire control system had t remendous influences on aircraft design. The main technique connotation and appr oaches of new integrated adaptive flight control system were introduced.
作者 张汝麟
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2003年第12期1077-1083,共7页 Journal of Beijing University of Aeronautics and Astronautics
关键词 飞行控制 主动控制技术 电传飞行控制系统 射流矢量推力 创新的控制效应器 flight control active control technology fly-by-wire fluidic thr ust-vectoring innovative flight control effector
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参考文献14

  • 1Patterson D W. In pursuit of wings: The Wright brothers decide to fly[DB/OL]. http: //www.news-record.com /ae/firstflight/3 wright 22. htm,1999-08-22
  • 2李明,张汝麟. 我国飞机主动控制技术的开发与验证[A]. 见:庄逢甘,郑哲敏主编. 钱学森技术科学思想与力学[C].北京:国防工业出版社,2001.84~91Li Ming,Zhang Rulin. Development and demonstration of aircraft active control technology in China [A]. In: Zhuang Fenggan, Zheng Zhemin, eds.Qian Xuesen' Technical Science Ideology and Mechanics[C]. Beijing: National Defense Industry Press,2001. 84~91(in Chinese)
  • 3张汝麟. 我国数字电传飞行控制技术的发展[A]. 见:面向新世纪的中国航空[C]. 北京:中国航空学会,2001Zhang Rulin. Development of digital fly-by-wire flight control technology in China [A]. In: Chinese Aviation Faced to the New Century[C]. Beijing: Chinese Society of Aeronautics and Astronautics, 2001(in Chinese)
  • 4张汝麟. 飞行控制系统[A]. 见:顾诵芬主编.蓝天雄鹰探秘[C]. 济南:山东教育出版社,2001.242~265Zhang Rulin. Flight control system [A]. In: Gu Songfen,ed. Secrecy Exploration of Sky Hawk [C]. Jinan: Shandong Education Press, 2001. 242~265 (in Chinese)
  • 5张汝麟.主动控制与综合控制[J].飞行力学,1997,15(3):1-6. 被引量:4
  • 6Boeing-Phantom Works. Future aircraft technology enhancement-block 1-Phase 1 [DB/OL]. http: //www. fas.org/man/dod-101/sys/ac/docs/bfrptpa4/tsld001.htm, 1997
  • 7Lockheed-Martin. Future aircraft technology enhancement, FATE 1 Phase 1, Final Report. [DB/OL]. http: //www. fas.org/man/dod-101/sys/ac/docs/fate report/index.htm, 1997-09-24
  • 8David J Wing. Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle[R]. NASA TM-4574,1994
  • 9Deere K A. PAB3D simulations of a nozzle with fluidic injection for yaw thrust-vector control[R].AIAA 98-3254,1998
  • 10Flamm J D. Experimental study of a nozzle using fluidic counterflow for thrust vectoring[R]. AIAA 98-3255,1998

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