Optimization Study of High Altitude Micro Gliding Air Vehicle Re-Entry Path Characteristics

Zhengyu Qu; Yanchu Yang; Feng Yan

doi:10.1051/jnwpu/20193750983

All issues

Volume 37 / No 5 (October 2019)

JNWPU, 37 5 (2019) 983-991

References

Open Access

Issue		JNWPU Volume 37, Number 5, October 2019


Page(s)		983 - 991
DOI		https://doi.org/10.1051/jnwpu/20193750983
Published online		14 January 2020

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[1] XiaoYongli, Zhang Chen. Study on Present Situation and Development of Micro Air Vehicles[J]. Journal of Astronautics, 1992, 18(5): 585–589 [Article] [Google Scholar]

[2] Hundley R O, Gritton E C. Future Technology-Driven Revolutions in Military Operations[R]. DB-110-ARPA, 1994 [Google Scholar]

[3] Waszak M R, Davidson J B, Ifju P G. Simulation and Flight Control of an Aeroelastic Fixed Wing Micro Aerial Vehicle[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit, Monterey, CA, 2002 [Google Scholar]

[4] Grasmeyer J, Keennon M. Development of the Black Widow Micro Air Vehicle[C]//AIAA 39th Aerospace Sciences Meeting and Exhibit, Reno, NV, 2001 [Google Scholar]

[5] Kahn A, Edwards D. Navigation, Guidance and Control for the Cicada Expendable Micro Air Vehicle[C]//AIAA Guidance, Navigation and Control Conference, 2012 [Google Scholar]

[6] Edwards D J, Kahn A D, Heinzen S B, et al. CICADA Flying Circuit Board Unmanned Aerial Vehicle[C]//2018 AIAA Aerospace Sciences Meeting, 2018 [Google Scholar]

[7] Laiacker M, Wlach S, Schwarzbach M. DLR High Altitude Balloon Launched Experimental Glider(Hableg): System Design, Control and Flight Data Analysis[C]//Workshop on Research, 2016 [Google Scholar]

[8] Yan Xiaodong, Tang San. Applying Pseudo-Spectral Method to Optimizing Entry Trajectory of Suborbital Launch Vehicle[J]. Journal of Northwestern Polytechnical University, 2010, 28(5): 748–752 [Article] [Google Scholar]

[9] Chen Xiaoqing, Hou Zhongxi, Liu Jianxia. Trajectory Characteristic of Hypersonic Gliding Vehicle[J]. Missiles and Space Vehicles, 2011, (2): 5–9 [Article] [Google Scholar]

[10] Li Ghuanghua, Zhang Hongbo, Tang Guojian. Typical Trajectory Characteristics of Hypersonic Glide Vehicle[J]. Journal of Astronautics, 2015, 36(4): 397–403 [Article] [Google Scholar]

[11] Gao Xianzhong. Research on High-Altitude Long-Endurance Flight of Solar-Powered Aircraft Based on Gravitational Potential and Wind Shear[D]. Hefei, National University of Defense Technology, 2014 (in Chinese) [Google Scholar]

[12] Shkarayev S V, Ifju P G, Kellogg J C, et al. Introduction to the Design of Fixed-Wing Micro Air Vehicles Including Three Case Studies[M]. American Institute of Aeronautics and Astronautics, 2007 [CrossRef] [Google Scholar]

[13] Vinh N X. Optimal Trajectories in Atmospheric Flight[M]. New York, Elsevier Scientific Publishing Company, 1981 [Google Scholar]

[14] Torres G E, Mueller T J. Low Aspect Ratio Aerodynamics at Low Reynolds Numbers[J]. AIAA Journal, 2004, 42(5): 865–873 [Article] [NASA ADS] [CrossRef] [Google Scholar]

[15] Pelletier A, Mueller T J. Low Reynolds Number Aerodynamics of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate Wings[J]. Journal of Aircraft, 2012, 37(5): 825–832 [Article] [CrossRef] [Google Scholar]

[16] Ananda G K, Sukumar P P, Selig M S. Measured Aerodynamic Characteristics of Wings at Low Reynolds Numbers[J]. Aerospace Science and Technology, 2015, 42: 392–406 [Article] [CrossRef] [Google Scholar]

[17] Okamoto M, Azuma A. Aerodynamic Characteristics at Low Reynolds Numbers for Wings of Various Planforms[J]. AIAA Journal, 2011, 49(6): 1135–1150 [Article] [NASA ADS] [CrossRef] [Google Scholar]

[18] Zipfel P H. Modeling and Simulation of Aerospace Vehicle Dynamics[M]. American Institute of Aeronautics and Astronautics, 2007 [CrossRef] [Google Scholar]

[19] Han Zipeng. Exterior Ballistics of Projectiles and Rockets[M]. Beijing, Beijing Institute of Technology Press, 2014 [Google Scholar]

[20] Ferreira L O. Nonlinear Dynamics and Stability of Hypersonic Reentry Vehicles[D]. Michigan, University of Michigan, 1995 [Google Scholar]

[21] Polhamus E C. Predictions of Vortex-Lift Characteristics by a Leading-Edge-Suction Analogy[J]. Journal of Aircraft, 1971, 8(4): 193–199 [Article] [CrossRef] [Google Scholar]