[115]胡江波, 梁宪珠, 张铖, 等. 高载荷质量比复合材料机翼模型结构设计与制造研究[J]. 材料开发与应用, 2011, 26(3): 41
HU Jiangbo, LIANG Xianzhu, ZHANG Cheng, et al. Study on structure design and manufacture of high load-weight ratio composite wing model[J]. Development and Application of Materials, 2011, 26(3): 41. DOI: 10.19515/j.cnki.1003-1545.2011.03.011
[116]向锦武, 李道春, 赵仕伟, 等. 一种复合材料机翼防固化变形模具设计: 201810151683.9[P]. 2018-08-31
[117]向锦武, 李道春, 张雪娇, 等. 一种复合材料机翼开口补强的优化设计方法: 201810146327.8[P]. 2018-09-04
[118]张健. 柔性飞机非线性气动弹性与飞行动力学耦合建模与仿真[D]. 北京：北京航空航天大学, 2010
ZHANG Jian. Modeling and simulation of coupled nonlinear aeroelasticity and flight dynamics for flexible aircraft[D].Beijing: Beihang University, 2010
[119]WASZAK M R, SCHMIDT D K. Flight dynamics of aeroelastic vehicles[J]. Journal of Aircraft, 1988, 25(6): 563. DOI: 10.2514/3.45623
[120]BUTTRILL C S, ARBUCKLE P D, ZEILER T A. Nonlinear simulation of a flexible aircraft in maneuvering flight[C]//Proceedings of the AIAA Flight Simulation Technologies Conference. Monterey, CA: AIAA, 1987: 122. DOI: 10.2514/6.1987-2501
[121]MEIROVITCH L, TUZCU I. Unified theory for the dynamics and control of maneuvering flexible aircraft[J]. AIAA Journal, 2004, 42(4): 714. DOI: 10.2514/1.1489
[122]DAMVELD H, MULDER J A. Influence of instationary aerodynamics and trimming on the dynamics of an aeroelastic aircraft[C]//Proceedings of the AIAA Modeling and Simulation Technologies Conference, San Francisco, CA: AIAA, 2005: 1. DOI: 10.2514/6.2005-6334
[123]SILVESTRE F J, PAGLIONE P. Dynamics and control of a flexible aircraft[C]//Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit. Honolulu, Hawaii: AIAA, 2008: 1. DOI: 10.2514/6.2008-6876
[124]PATIL M J, HODGES D H, CESNIK C E S. Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft[J]. Journal of Aircraft, 2001, 38(1): 88. DOI: 10.2514/2.2738
[125]肖伟, 周洲, 祝小平, 等. 高空太阳能无人机飞行动力学建模与分析[J]. 飞行力学, 2012, 30(5): 385
XIAO Wei, ZHOU Zhou, ZHU Xiaoping, et al. Modelling and analysis on flight dynamics of high altitude solar UAV[J]. Flight Dynamics, 2012, 30(5): 385.DOI:10.13645/j.cnki.f.d. 2012.05.004
