飞行控制与飞机发展

张汝麟

飞行控制与飞机发展

张汝麟

飞行自动控制研究所, 西安 710065

详细信息

作者简介:
张汝麟(1937-),男,河南洛阳人,研究员, rlzhang@facri.com.

中图分类号: V 249.1
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- 被引次数: 0
出版历程
- 收稿日期: 2003-06-20
- 网络出版日期: 2003-12-31

Development of flight control with aircraft

Zhang Rulin

Flight Automatic Control Research Institute, Xi'an 710065, China

摘要

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20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.重点介绍了新型综合自适应飞行控制系统的主要技术内涵和实现途径.
- 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
Abstract: 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 tremendous influences on aircraft design. The main technique connotation and approaches of new integrated adaptive flight control system were introduced.
- flight control /
- active control technology /
- fly-by-wire /
- fluidic thrust-vectoring /
- innovative flight control effector

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参考文献(1)

[1] Patterson D W. In pursuit of wings:The Wright brothers decide to fly. 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. 见:庄逢甘,郑哲敏主编. 钱学森技术科学思想与力学. 北京:国防工业出版社,2001.84~91 Li Ming,Zhang Rulin. Development and demonstration of aircraft active control technology in China. In:Zhuang Fenggan, Zheng Zhemin, eds.Qian Xuesen' Technical Science Ideology and Mechanics. 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. 见:面向新世纪的中国航空. 北京:中国航空学会,2001 Zhang Rulin. Development of digital fly-by-wire flight control technology in China. In:Chinese Aviation Faced to the New Century. Beijing:Chinese Society of Aeronautics and Astronautics, 2001(in Chinese) [4] 张汝麟. 飞行控制系统. 见:顾诵芬主编.蓝天雄鹰探秘. 济南:山东教育出版社,2001.242~265 Zhang Rulin. Flight control system. In:Gu Songfen,ed. Secrecy Exploration of Sky Hawk. 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 Zhang Rulin. Active control and integrated control technologies[J]. Flight Dynamics, 1997,15(3):1~6 (in Chinese) [6] Boeing-Phantom Works. Future aircraft technology enhancement-block 1-Phase 1. http:// www. fas.org/man/dod-101/sys/ac/docs/bfrptpa4/tsld001.htm, 1997. [7] Lockheed-Martin. Future aircraft technology enhancement, FATE 1 Phase 1, Final Report. http:// www. fas.org/man/dod-101/sys/ac/docs/fate report/index.htm, 1997-09-24. [8] David J Wing. Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle. NASA TM-4574,1994. [9] Deere K A. PAB3D simulations of a nozzle with fluidic injection for yaw thrust-vector control. AIAA 98-3254,1998. [10] Flamm J D. Experimental study of a nozzle using fluidic counterflow for thrust vectoring. AIAA 98-3255,1998. [11] Fisher D F, Murri D G. Forebody flow visualization on the F-18 HARV with actuated forebody strakes. NASA TM-1998-206556,1998. [12] Rediniotis O K, Lagoubas D C, Garner L, et al. Experiments and analysis of an active hydrofoil with SMA actuators. AIAA 98-0102,1998. [13] Scott M A, Monlgomery R C, Weston R P. Subsonic maneuvering effectiveness of high performance aircraft which employ quasi-static shape change devices. In:SPIE 5th Annual International Symposium on Smart Structure and Materials, 1998. [14] Raney D L, Monlgomery R C, Green L L. Flight control using distributed shape-change effector arrays. AIAA 2000-1560, 2000

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