Open Access
Issue |
JNWPU
Volume 38, Number 3, June 2020
|
|
---|---|---|
Page(s) | 523 - 532 | |
DOI | https://doi.org/10.1051/jnwpu/20203830523 | |
Published online | 06 August 2020 |
- Greg A D. Profile-Following Entry Guidance Using Linear Quadratic Regulator Theory[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit, Monterey, 2002 [Google Scholar]
- Curtis Z, Greg D, John H. An Automated Method to Compute Orbital Reentry Trajectories with Heating Constraints[J]. Journal of Guidance, Control, and Dynamics, 2003, 26(4): 523-529 [Article] [CrossRef] [Google Scholar]
- Wang Jinbo, Cui Naigang, Guo Jifeng, et al. High Precision Rapid Trajectory Optimization Algorithm for Launch Vehicle Landing[J]. Control Theory & Applications, 2018, 35(3): 389-398 [Article] (in Chinese) [Google Scholar]
- Hamel J F, Lafontaine J D. Improvement to the Analytical Predictor-Corrector Guidance Algorithm Applied to Mars Aerocpture[J]. Journal of Guidance, Control, and Dynamics, 2006, 29(4): 1019-1022 [Article] [CrossRef] [Google Scholar]
- Lu P. Entry Guidance:A Unified Method[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(3): 713-728 [Article] [CrossRef] [Google Scholar]
- Wang Zhi, Tang Shuo, Yan Xiaodong. Constrained Predictor-Corrector Reentry Guidance for Hypersonic Glide Vehicle[J]. Flight Dynamics, 2012, 30(2): 175-180 [Article] (in Chinese) [Google Scholar]
- Liang Zixuan, Ren Zhang. Predictive Reentry Guidance with Aerodynamic Parameter Online Correction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(7): 853-857 [Article](in Chinese) [Google Scholar]
- Wang Zhi, Zhang Ran, Li Huifeng. Hybrid Re-Entry Guidance for Reusable Launch Vehicle[C]//2014 Asia-Pacific International Symposium on Aerospace Technology, 2015: 999-1004 [Google Scholar]
- Song Jianshuang, Hu Yu, Hong Bei, et al. Predictor-Corrector Guidance for Common Aero Vehicle[J]. Missiles and Space Vehicles, 2016, 348(34): 38[Article] (in Chinese) [Google Scholar]
- Cheng Yang, Cheng Lin, Zhang Qingzhen, et al. Aircraft Predictor-Corrector Guidance Based on Online Constraint Limit Enforcement[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 2143-2153 [Article] (in Chinese) [Google Scholar]
- Wang Qing, Ran Maopeng, Zhao Yang. Reentry Guidance for Hypersonic Vehicle Based on Predictor-Corrector Method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(12):1563-1567 [Article](in Chinese) [Google Scholar]
- Ran Maopeng, Wang Qing, Mo Huadong, et al. ANFIS-Based Predictive Reentry Guidance for Hypersonic Vehicles[J]. Acta Armamentarii, 2014, 35(12): 2016-2022 [Article] (in Chinese) [Google Scholar]
- Yong Enmi, Qian Weiqi, He Kaifeng. An Adaptive Predictor-Corrector Reentry Guidance Based on Self-Definition Way-Points[J]. Aerospace Science and Technology, 2014, 39:211-221 [Article] [CrossRef] [Google Scholar]
- Li Huifeng, Xie Ling. Reentry Guidance Law Design for RLV Based on Predictor-Corrector Method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(11): 1344-1348 [Article](in Chinese) [Google Scholar]
- Zhao Jiang, Zhou Rui. Predictor-Corrector Reentry Guidance Based on Feedback Bank Angle Control[J]. Acta Armamentarii, 2015, 36(5): 823-830 [Article] (in Chinese) [Google Scholar]
- Shen Zuojun, Lu Ping. Dynamic Lateral Entry Guidance Logic[J]. Journal of Guidance, Control, and Dynamics, 2004, 27(6): 949-959 [Article] [CrossRef] [Google Scholar]
- Lu Ping. Predictor-corrector Entry Guidance for Low Lifting Vehicles[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit, Hilton Head, South Carolina, 2007: 6425 [Google Scholar]
- Xue Songbai, Lu Ping. Constrained Predictor-Corrector Entry Guidance[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(4): 1273-1281 [Article] [CrossRef] [Google Scholar]
- Guo Jifeng, Fu Yu, Cui Naigang. Three Dimensional Autonomous Entry Guidance Method[J]. Control and Decision, 2013, 28(5): 688-694 [Article] [Google Scholar]
- Wang Tao, Zhang Hongbo, Zhu Ruyi, et al. Predictor-Corrector Reentry Guidance Based on Drag Acceleration[J]. Journal of Astronautics, 2017, 38(2): 143-151 [Article] (in Chinese) [Google Scholar]
- Hu Zhengdong. Research on Trajectory Planning and Guidance for Space-Based Strike Weapon[D]. Changsha: National University of Defense Technology, 2009(in Chinese) [Google Scholar]
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