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All issues Volume 43 / No 4 (August 2025) JNWPU, 43 4 (2025) 668-676 References
Open Access
Issue
JNWPU
Volume 43, Number 4, August 2025
Page(s) 668 - 676
DOI https://doi.org/10.1051/jnwpu/20254340668
Published online 07 October 2025
  1. ZHOU Ping, ZHAO Chenxiao, MEI Lin, et al. Development situation and trends analysis of modern tank active p rotection system[J]. Command Control & Simulation, 2016, 38(2): 132–136 (in Chinese) [Google Scholar]
  2. REN Baoquan. Research on field command post site selection and its module solving[D]. Changsha: National University of Defense Technology, 2010 (in Chinese) [Google Scholar]
  3. WANG S, WANG W, XIONG S. Impact angle constrained three-dimensional integrated guidance and control for STT missile in the presence of input saturation[J]. ISA Transactions, 2016, 64: 151–160 [Article] [Google Scholar]
  4. SONG J, SONG S. Three-dimensional guidance law based on adaptive integral sliding mode control[J]. Chinese Journal of Aeronautics, 2016, 29(1): 202–214 [Article] [Google Scholar]
  5. SONG J, SONG S. Robust impact angle constraints guidance law with autopilot lag and acceleration saturation consideration[J]. Transactions of the Institute of Measurement and Control, 2019, 41(1): 182–192 [Article] [Google Scholar]
  6. JIANG S, TIAN F, SUN S, et al. Integrated guidance and control of guided projectile with multiple constraints based on fuzzy adaptive and dynamic surface[J]. Defence Technology, 2020, 16(6): 1130–1141 [Article] [Google Scholar]
  7. HU Q, HAN T, XIN M. Three-dimensional guidance for various target motions with terminal angle constraints using twisting control[J]. IEEE Trans on Industrial Electronics, 2019, 67(2): 1242–1253 [Google Scholar]
  8. HU Q, HAN T, XIN M. Analytical solution for nonlinear three-dimensional guidance with impact angle and field-of-view constraints[J]. IEEE Trans on Industrial Electronics, 2020, 68(4): 3423–3433 [Google Scholar]
  9. GUO Zhengyu, WANG Chaolei, QIAN Hang, et al. Cooperative intercepting guidance law for large maneuvering target with impact angle constraint[J]. Journal of Northwestern Polytechnical University, 2020, 38(6): 1257–1265 [Article][Article] (in Chinese) [Google Scholar]
  10. WANG X, LU H, HUANG X, et al. Three-dimensional terminal angle constraint finite-time dual-layer guidance law with autopilot dynamics[J]. Aerospace Science and Technology, 2021, 116(1): 106818 [Google Scholar]
  11. LI T, QIAN H M. Three-dimensional impact angles constrained integral sliding mode guidance law for missiles with input saturation[J]. Journal of Aerospace Engineering, 2022, 236(14): 2953–2962 [Google Scholar]
  12. YANG X, ZHANG Y, SONG S. Three-dimensional nonsingular impact angle guidance strategy with physical constraints[J]. ISA Transactions, 2022, 131476–488 [Article] [Google Scholar]
  13. WANG Yuchen, WANG Wei, LIN Shiyao, et al. Three-dimensional adaptive sliding mode cooperative guidance law with impact time and angle constraints[J]. Acta Armamentarii, 2023, 44(9): 2778–2790 (in Chinese) [Google Scholar]
  14. ZHANG Z L, ZHANG K, HAN Z G. Incremental nonlinear dynamic inverse-adaptive sliding mode three-dimensional angle constrained guidance law design[J]. IEEE Trans on Aerospace and Electronic Systems, 2024, 60(1): 186–201 [Article] [Google Scholar]
  15. MA Dengwu, LIU Yan, TIAN Zhenhua. Survey on over the shoulder of air-to-air missile[J]. Journal of Naval Aviation University, 20073): 377–381 (in Chinese) [Google Scholar]
  16. ZHANG X C, XU L, WANG J, et al. Research on multiple loitering munitions trajectory planning method[C]//IEEE 2023 International Conference on Cyber-Physical Social Intelligence, Xi'an, China, 2023 [Google Scholar]
  17. GAO Jinsong, ZHAO Huachao, TIAN Xingmin. On relationship between two modes of AAM's all-aspect attack[J]. Electrooptics and Control, 2018, 25(12): 16–20 (in Chinese) [Google Scholar]
  18. CUI Yankai, WANG Zhigang. Aerodynamic and thrust vector complex controller design of over the shoulder air-to-air missile[J]. Journal of Astronautics, 2010, 31(4): 1100–1104 (in Chinese) [Google Scholar]
  19. WEI Yali, YIN Wei, LIU Yintian, et al. Research on big off-axis turning law under multiple constraints for agile missile[J]. Air & Space Defense, 2020, 3(3): 96–102 (in Chinese) [Google Scholar]
  20. ZHANG Peng, ZHANG Jinpeng. Research on guidance law of over the shoulder air-to-air missile[J]. Aero Weaponry, 20143): 8–11 (in Chinese) [Google Scholar]
  21. LI Ruikang, CHEN Miao, ZHONG Yongjian. Optimal design of guidance law for missile launch with large off-axis angle[J]. Aerospace Control, 2024, 42(1): 58–64 (in Chinese) [Google Scholar]
  22. ZHANG Qian, ZHOU Hao, GUO Zuhua. Trajectory design of air-to-air missile's agile turn with reaction jets control[J]. Tactical Missile Technology, 20183): 38–43 (in Chinese) [Google Scholar]
  23. WISE K, SEDWICK J. Nonlinear H(infinity) optimal control for agile missiles[C]//IEEE Conference on Decision and Control, Florence, 2013 [Google Scholar]
  24. RIDGELY D, DRAKE D, TRIPLETT L, et al. Dynamic control allocation of a missile with tails and reaction jets[C]//AIAA Guidance, Navigation and Control Conference, Boston, Massachusetts, USA, 2013 [Google Scholar]
  25. YANG K, XU C, XU Y. Design and implementation of trajectory planning algorithm for UAV borne air-to-surface missile[J]. Journal of Physics: Conference Series, 2021, 1721(1): 012038 [Google Scholar]
  26. ZHOU L Y, XIA Y Q. Improved ZEM/ZEV feedback guidance for Mars powered descent phase[J]. Advances in Space Research, 2014, 54(11): 2446–2455 [Google Scholar]
  27. TANG Jingyuan, GOU Yongjie, MA Yangyang, et al. Rocket landing guidance based on second-order Picard-Chebyshev-Newton type algorithm[J]. Journal of Northwestern Polytechnical University, 2024, 42(1): 98–107 [Article] (in Chinese) [Google Scholar]
  28. YOU S X, WAN C H, DAI R, et al. Learning-based onboard guidance for fuel-optimal powered descent[J]. Journal of Guidance Control and Dynamics, 2020, 44(2): 601–613 [Google Scholar]
  29. ZHANG Wenjie, RUAN Cong, XIA Qunli, et al. Design of missile active disturbance rejection attitude control system[J]. Tactical Missile Technology, 20196): 67–73 (in Chinese) [Google Scholar]

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