Open Access
Issue
JNWPU
Volume 39, Number 2, April 2021
Page(s) 249 - 257
DOI https://doi.org/10.1051/jnwpu/20213920249
Published online 09 June 2021
  1. TahkM, ParkC S, RyooC K. Line-of-sight guidance laws for formation flight[J]. Journal of Guidance, Control and Dynamics, 2005, 28(4): 708–716 [Article] [Google Scholar]
  2. DoganA, VenkataramananS. Nonlinear control for reconfiguration of unmmaned-aerial-vehicle formation[J]. Journal of Guidance, Control and Dynamics, 2005, 28(4): 667–678 [Article] [Google Scholar]
  3. Giulietti F, Innocenti M, Napolitano M, et al. Dynamic and control issues of formation flight[J]. Aerospace Science and Technology, 2005, 9: 65–71 [Article] [Google Scholar]
  4. Ajoulou A, Moezzi K, Aghdan A G, et al. Two-stage energy-optimal formation reconfiguration strategy[J]. Automatica, 2012, 48: 2587–2591 [Article] [Google Scholar]
  5. AjorlouA, MoezziK, AghdamA G, et al. Two-stage time-optimal formation reconfiguration strategy[J]. System & Control Letters, 2013, 62: 496–502 [Article] [Google Scholar]
  6. Zhao Weihua, Go T H. Quadcopter formation flight control combining MPC and robust feedback linearization[J]. Journal of the Fronklin Institute, 2014, 351(3): 1335–1355 [Article] [Google Scholar]
  7. Jiang Zeyu, Cheng Hui, Zheng Zefeng, et al. Autonomous formation flight of UAVs: control algorithms and field experiments[C]//Proceedings of the 35th Chinese Control Conferece, 2016 [Google Scholar]
  8. Wei Yang, Xu Haojun, Xue Yuan. Adaptive disturbance rejection controller design for UAV three dimensional formation keeping[J]. Systems Engineering and Electronics, 2018, 40(12): 2758–2765 [Article] (in Chinese) [Google Scholar]
  9. Xie Wenguang, Wu Kang, Yan Fang, et al. A Formation flight method with an improved deep neural network for multi-UAV system[J]. 2020, 38(2): 295–302 (in Chinese) [Google Scholar]
  10. Wang Jianying, Sun Zhaowei. 6-DOF robust terminal sliding mode control for spacecraft formation flying[J]. Acta Astronautica, 2012, 73: 76–87 [Article] [Google Scholar]
  11. Ma Peibei, Ji Jun. Three-dimensional multi-missile formation control[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(8): 1660–1666 [Article] (in Chinese) [Google Scholar]
  12. Wei Changzhu, Guo Jifeng, Cui Naigang. Research on the missile formation keeping optimal control for cooperative engagement[J]. Journal of Astronautics, 2010, 31(4): 1043–1050 [Article] (in Chinese) [Google Scholar]
  13. Zhang Lei, Fang Yangwang, Mao Donghui, et al. Adaptive sliding-mode controller design for missile cooperative engagement[J]. Journal of Astronautics, 2014, 35(6): 700–707 [Article] (in Chinese) [Google Scholar]
  14. Zhang Lei, Fang Yangwang, Diao Xinghua, et al. Design of nonlinear optimal controller for multi-missile formation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 401–406 [Article] (in Chinese) [Google Scholar]
  15. Zhou Huibo, Song Shenmin, Zheng Zhong. Distributed robust adaptive control for missile cooperative engagement within formation[J]. Journal of Chinese Inertial Technology, 2015, 23(4): 516–527 [Article] (in Chinese) [Google Scholar]
  16. Peng Mingxing, Wu Yunjie, Zhu Futao. Research on control method for anti-ship missiles formation flight[J]. Journal of System Simulation, 2017, 29(1): 212–217 [Article] (in Chinese) [Google Scholar]
  17. Xiong Ke, Guo Zhenyun. A variable structure terminal guidance law of anti-mobile missile in atmosphere[C]. //Proceedings of the Annual Conference of Flight Mechanics and Flight Test Academic Exchange, 2006 (in Chinese) [Google Scholar]
  18. Liu Jinkun. Sliding mode control design and MATLAB simulation[M]. [3rd Edition]. Beijing: Tsinghua University Press, 2015 [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.