[1] |
Hongyan ZHANG, Wei WANG, Shiwei CHEN, Yi JI, Jiaqi LIU.
Integrated guidance and control design based on fully actuated system method
[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628891-628891.
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[2] |
Yongzhi SHENG, Jiahao GAN, Chengxin ZHANG.
Fractional order sliding mode guidance law design with trajectory adjustable and terminal angular constraint
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 327073-327073.
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[3] |
Haowen LUO, Shaoming HE, Tianyu JIN, Zichao LIU.
Impact-angle-constrained with time-minimum guidance algorithm based on transfer learning
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 328400-328400.
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[4] |
LIU Zichao, WANG Jiang, HE Shaoming, LI Yufei.
A computational guidance algorithm for impact angle control based on predictor-corrector concept
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 325433-325433.
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[5] |
WANG Yaning, WANG Hui, LIN Defu, YUAN Yifang.
Guidance method for maneuvering target interception based on virtual look angle constraint
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 324799-324799.
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[6] |
LI Kebo, LIAO Xuanping, LIANG Yan'gang, LI Chaoyong, CHEN Lei.
Guidance strategy with impact angle constraints based on pure proportional navigation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S2): 724277-724277.
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[7] |
JIANG Peng, GUO Dong, HAN Liang, LI Qingdong, REN Zhang.
Trajectory optimization for cooperative reentry of multiple hypersonic glide vehicle
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S1): 723776-723776.
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[8] |
LI Xiaobao, ZHAO Guorong, ZHANG Youan, GUO Zhiqiang.
Adaptive nonsingular terminal sliding mode guidance law with strict convergence
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(5): 322569-322569.
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[9] |
LI Chendi, WANG Jiang, LI Bin, HE Shaoming, ZHANG Tong.
Energy-optimal guidance law with virtual hand-over point
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(12): 323249-323249.
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[10] |
ZHANG Kuanqiao, YANG Suochang, LI Baochen, LIU Chang.
Fixed-time convergent guidance law considering autopilot dynamics
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(11): 323227-323227.
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[11] |
DUAN Meijun, ZHOU Di, CHENG Dalin.
Development of terminal guidance law and PWPF modulator for near space interceptor based on finite time theory
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(1): 321481-321481.
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[12] |
GUO Jianguo, HAN Tuo, ZHOU Jun, WANG Guoqing.
Second-order sliding-mode guidance law with impact angle constraint
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(2): 320208-320217.
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[13] |
ZHAO Qilun, CHEN Jian, LI Qingdong, REN Zhang, LI Liang.
Feasible region of hypersonic and ballistic missiles' cooperative attack strategy
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(7): 2291-2300.
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[14] |
ZHANG Siyu, YU Jianqiao, LI Pinlei.
Multiple ballistic flight vehicles' launch time planning for collision avoidance based on time constraint set
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(7): 2391-2399.
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[15] |
ZHANG Youan, HUANG Jie, SUN Yangping.
Generalized Weighted Optimal Guidance Laws with Impact Angle Constraints
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(3): 848-856.
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