[1] Simon J M,Blake W B,Multhopp D. Control concepts for a vertical tailless fighter. AIAA-1993-4000,1993: 1-11.
[2] Bowlus J A,Multhopp D,Banda S S. Challenges and opportunities in tailless aircraft stability and control. AIAA-1997-3830,1997: 1713-1718.
[3] Goodall J. B-2 spirit in action[M]. Carrollton Texas: Squadron/Signal Publications,2002: 7-12.
[4] 张子军,黎军,李天,等. 开裂式方向舵对某无尾飞翼布局飞机气动特性影响的实验研究[J]. 实验流体力学,2010,24(3): 63-66. Zhang Zijun,Li Jun,Li Tian,et al. Experimental investigation of split-rudder deflection on aerodynamic per-formance of tailless flying-wing aircraft[J]. Journal of Experiments in Fluid Mechanics,2010,24(3): 63-66. (in Chinese)
[5] 马超,李林,王立新. 大展弦比飞翼布局飞机新型操纵面设计[J]. 北京航空航天大学学报,2007,33(2): 149-153. Ma Chao,Li Lin,Wang Lixin. Design of innovative control surfaces of flying wing aircrafts with large ratio aspect[J]. Journal of Beijing University of Aeronautics and Astronautics,2007,33(2): 149-153. (in Chinese)
[6] 王睿,祝小平,周洲,等. 阻力方向舵在飞翼式高空长航时无人机中的应用[J]. 西北工业大学学报,2008,26(6): 673-677. Wang Rui,Zhu Xiaoping,Zhou Zhou,et al. Exploring utilization of drag rudder in stability and control of flying wing high altitude long endurance(HALE)UAV[J]. Journal of Northwestern Polytechnical University,2008,26(6): 673-677. (in Chinese)
[7] 马松辉,吴成富,陈怀民. 阻力方向舵在无尾飞机飞行控制中的应用[J]. 飞行力学,2008,26(2): 69-73. Ma Songhui,Wu Chengfu,Chen Huaimin. The applica-tion of drag rudder to flight control of tailless aircraft[J]. Flight Dynamics,2008,26(2): 69-73. (in Chinese)
[8] 李林,王立新. 大展弦比飞翼作战飞机横航向飞行品质特性[J]. 北京航空航天大学学报,2009,35(6): 661-664. Li Lin,Wang Lixin. Lateral-directional flying quality characteristics of high aspect-ratio combat flying wings[J]. Journal of Beijing University of Aeronautics and Astronautics,2009,35(6): 661-664. (in Chinese)
[9] 方振平,陈万春,张曙光. 航空飞行器飞行动力学[M]. 北京: 北京航空航天大学出版社,2005: 274. Fang Zhenping,Chen Wanchun,Zhang Shuguang. Aircraft flight dynamics[M]. Beijing: Beihang University Press,2005: 274. (in Chinese)
[10] 李林,马超,王立新. 大展弦比飞翼构型的横航向操纵特性[J]. 北京航空航天大学学报,2007,33(10): 1186-1190. Li Lin,Ma Chao,Wang Lixin. Lateral-directional control characteristics of high aspect-ratio flying wing configurations[J]. Journal of Beijing University of Aeronautics and Astronautics,2007,33(10): 1186-1190. (in Chinese)
[11] 马超. 飞翼布局作战飞机可控性设计研究. 北京: 北京航空航天大学,2009. Ma Chao. Controllability design of flying-wing configuration combat aircraft. Beijing: Beihang University,2009. (in Chinese)
[12] Durham W C. Constrained control allocation. AIAA-1992-4550,1992: 1147-1155.
[13] Ito D,Georgie J,Valasek J,et al. Reentry vehicle flight controls design guidelines: dynamic inversion. NASA/TP-2002-210771,2002: 1-99.
[14] 柳嘉润,申功璋. 基于逆动力学与在线参数辨识的飞机姿态控制[J]. 北京航空航天大学学报,2005,31(2): 111-115. Liu Jiarun,Shen Gongzhang. Attitude control based on inverse dynamics and online parameter identification[J]. Journal of Beijing University of Aeronautics and Astro-nautics,2005,31(2): 111-115. (in Chinese)
[15] 王磊,王立新,贾重任. 多操纵面飞翼布局作战飞机的控制分配方法[J]. 航空学报, 2011, 32(4): 571-579. Wang Lei,Wang Lixin,Jia Zhongren. Control allocation method for combat flying wing with multiple control surfaces[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(4): 571-579. (in Chinese) |