Development of flight control with aircraft

[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