Open Access
Issue
JNWPU
Volume 44, Number 1, February 2026
Page(s) 143 - 150
DOI https://doi.org/10.1051/jnwpu/20264410143
Published online 27 April 2026
  1. Xie L, Zhang Y, Xu J. Optimal two-impulse space interception with multiple constraints[J]. Frontiers of Information Technology & Electronic Engineering, 2020, 21(7): 1085–1107 [Google Scholar]
  2. Tu Fanqing, Yang Hongwei. Trajectory optimization method for low-thrust collision avoidance under J2 perturbation[J]. Flight Control & Detection, 2025, 8(2): 27–39 (in Chinese) [Google Scholar]
  3. Han Yaokun, Chen Qifeng. Orbit design and simulation of omnidirectional long-term formation-flying satellite clusters[J]. Flight Control & Detection, 2020, 3(3): 33–39 (in Chinese) [Google Scholar]
  4. Xu Hao, Deng Xin, Liao Xueyang, et al. A review of SDRE control methods for spacecraft[J]. Flight Control & Detection, 2024, 7(5): 30–49 (in Chinese) [Google Scholar]
  5. Shen H, Tsiotras P. Using battin′s method to obtain multiple-revolution lambert′s solutions[J]. Advances in the Astronautical Sciences, 2003, 116: 1067–1084 [Google Scholar]
  6. Yang B, Li S, Feng J, et al. Fast solver for J2-perturbed lambert problem using deep neural network[J]. Journal of Guidance, Control, and Dynamics, 2022, 45(5): 875–884. [Article] [Google Scholar]
  7. Ottesen D, Russell R P. Unconstrained direct optimization of spacecraft trajectories using many embedded Lambert problems[J]. Journal of Optimization Theory and Applications, 2021, 191: 634–674. [Article] [Google Scholar]
  8. Ding W, Li X, Yang H. Research on minimum time interception problem with a tangent impulse under relative motion models[J]. International Journal of Aerospace Engineering, 2019, 2019: 8912835 [Google Scholar]
  9. Oghim S, Leeghim H, Kim D. Real-time spacecraft intercept strategy on J2-perturbed orbits[J]. Advances in Space Research, 2019, 63(2): 1007–1016. [Article] [Google Scholar]
  10. Du Xiangnan, Yang Zhen. An algorithm for solving spacecraft reachable domain with single-impulse maneuvering[J]. Chinese Journal of Theoretical and Applied Mechanics, 2020, 52(6): 1621–1631 (in Chinese) [Google Scholar]
  11. Luo Y Z, Shen H X, Huang A Y, et al. GTOC X: results and methods of National University of Defense Technology and Xi′an Satellite Control Center[C]//Proceedings of AAS/AIAA Astrodynamics Specialist Conference, 2019. [Google Scholar]
  12. Xia Cunyan, Zhang Gang, Geng Yunhai. Coplanar multi-target interception with a single impelse[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(3): 352–362 (in Chinese) [Google Scholar]
  13. Zhang G, Zhou D, Mortari D. Optimal two-impulse rendezvous using constrained multiple-revolution lambert solutions[J]. Celestial Mechanics and Dynamical Astronomy, 2011, 110(4): 305–317. [Article] [Google Scholar]
  14. Snyoll O, Sung-Hoon M, Henzeh L. Optimal spacecraft rendezvous by minimum velocity change and wait time[J]. Advances in Space Research, 2017, 60(6): 1188–1200. [Article] [Google Scholar]
  15. Luo Y Z, Li H Y, Tang G J. Hybrid approach to optimize a rendezvous phasing strategy[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(1): 185–191. [Article] [Google Scholar]
  16. Lu Zhengliang. Study on mass moment attitude control for fast orbit maneuver satellite[D]. Nanjing: Nanjing University of Science and Technology, 2018. (in Chinese) [Google Scholar]
  17. Sathiyanathan K, Lee R, Chesser H, et al. Solid propellant microthruster design for nanosatellite applications[J]. Journal of Propulsion and Power, 2011, 27(6): 1288–1294. [Article] [Google Scholar]
  18. Mueller J. Thruster options for microspacecraft-a review and evaluation of existing hardware and emerging technologies[C]//33rd Joint Propulsion Conference and Exhibit, 1997: 3058. [Google Scholar]
  19. Wei Pengtao, Lei Gang, Guo Hongna, et al. Orbit interception at virtual crossing point based on lambert transfer[J]. Flight Dynamics, 2012, 30(6): 556–559 (in Chinese) [Google Scholar]
  20. Kheldoun A, Bradai R, Boukenoui R, et al. A new golden section method-based maximum power point tracking algorithm for photovoltaic systems[J]. Energy Conversion and Management, 2016, 111: 125–136. [Article] [Google Scholar]

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