Systems Engineering and Electronics ›› 2022, Vol. 44 ›› Issue (10): 3213-3220.doi: 10.12305/j.issn.1001-506X.2022.10.26
• Guidance, Navigation and Control • Previous Articles Next Articles
Jia HUANG, Sijiang CHANG*
Received:
2021-08-03
Online:
2022-09-20
Published:
2022-10-24
Contact:
Sijiang CHANG
CLC Number:
Jia HUANG, Sijiang CHANG. Data-driven method based impact time and impact angle control guidance law[J]. Systems Engineering and Electronics, 2022, 44(10): 3213-3220.
1 |
TSALIK R , SHIMA T . Circular impact-time guidance[J]. Journal of Guidance, Control, and Dynamics, 2019, 42 (8): 1836- 1847.
doi: 10.2514/1.G004074 |
2 | TEKIN R , ERER K S , HOLZAPFEL F . Impact time control with generalized-polynomial range formulation[J]. Journal of Guidance, Control, and Dynamics, 2018, 41 (5): 1188- 1193. |
3 |
WANG P Y , GUO Y N , MA G F , et al. New differential geometric guidance strategies for impact-time control problem[J]. Journal of Guidance, Control, and Dynamics, 2019, 42 (9): 1982- 1992.
doi: 10.2514/1.G004229 |
4 | WANG J W , ZHANG R . Terminal guidance for a hypersonic vehicle with impact time control[J]. Journal of Guidance, Control, and Dynamics, 2018, 41 (8): 1789- 1797. |
5 |
CHO D , KIM H J , TAHK M J . Nonsingular sliding mode guidance for impact time control[J]. Journal of Guidance, Control, and Dynamics, 2016, 39 (1): 61- 68.
doi: 10.2514/1.G001167 |
6 |
RYOO C K , CHO H , TAHK M J . Optimal guidance laws with terminal impact angle constraint[J]. Journal of Guidance, Control, and Dynamics, 2005, 28 (4): 724- 732.
doi: 10.2514/1.8392 |
7 |
LIN L G , XIN M . Impact angle guidance using state-dependent (differential) riccati equation: unified applicability analysis[J]. Journal of Guidance, Control, and Dynamics, 2020, 43 (11): 2175- 2182.
doi: 10.2514/1.G005244 |
8 | 郭佳晖, 蒋滨安, 田宗浩. 带有攻击角和视场角约束的制导炮弹导引律设计[J]. 系统工程与电子技术, 2021, 43 (4): 1050- 1056. |
GUO J H , JIANG B A , TIAN Z H . Guidance law design of guided projectile with impact angle and field-of-view constraints[J]. Systems Engineering and Electronics, 2021, 43 (4): 1050- 1056. | |
9 |
LI H Y , WANG J , HE S M , et al. Nonlinear optimal impact-angle-constrained guidance with large initial heading error[J]. Journal of Guidance, Control, and Dynamics, 2021, 44 (9): 1663- 1676.
doi: 10.2514/1.G005868 |
10 | LEE C H , SEO M G . New insights into guidance laws with terminal angle constraints[J]. Journal of Guidance, Control, and Dynamics, 2018, 41 (8): 1828- 1833. |
11 |
LEE J I , JEON I S , TAHK M J . Guidance law to control impact time and angle[J]. IEEE Trans.on Aerospace and Electronic Systems, 2007, 43 (1): 301- 310.
doi: 10.1109/TAES.2007.357135 |
12 | ERER K S , TEKIN R . Impact time and angle control based on constrained optimal solutions[J]. Journal of Guidance, Control, and Dynamics, 2016, 39 (10): 2445- 2451. |
13 | 李斌, 林德福, 何绍溟, 等. 基于最优误差动力学的时间角度控制制导律[J]. 航空学报, 2018, 39 (11): 157- 167. |
LI B , LIN D F , HE S M , et al. Time and angle control guidance law based on optimal error dynamics[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39 (11): 157- 167. | |
14 |
ZHANG Y A , WANG X L , MA G X . Impact time control guidance law with large impact angle constraint[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2015, 229 (11): 2119- 2131.
doi: 10.1177/0954410014568466 |
15 |
ZHANG Y A , MA G M , LIU A L . Guidance law with impact time and impact angle constraints[J]. Chinese Journal of Aeronautics, 2013, 26 (4): 960- 966.
doi: 10.1016/j.cja.2013.04.037 |
16 |
CHEN Y D , WANG J N , SHAN J Y , et al. Cooperative guidance for multiple powered missiles with constrained impact and bounded speed[J]. Journal of Guidance, Control, and Dynamics, 2021, 44 (4): 825- 840.
doi: 10.2514/1.G005578 |
17 | 吴放, 常思江. 攻击时间和攻击角度控制的非奇异终端滑模制导律[J]. 哈尔滨工业大学学报, 2021, 53 (6): 93- 103. |
WU F , CHANG S J . Nonsingular terminal sliding mode guidance law of impact time and impact angle control[J]. Journal of Harbin Institute of Technology, 2021, 53 (6): 93- 103. | |
18 | CHEN X T , WANG J Z . Sliding-mode guidance for simultaneous control of impact time and angle[J]. Journal of Guidance, Control, and Dynamics, 2019, 42 (2): 392- 401. |
19 | KUMAR S R, GHOSE D. Impact time and angle control guidance[C]//Proc. of the AIAA Guidance, Navigation, and Control Conference, 2015. |
20 |
HU Q L , HAN T , XIN M . New impact time and angle guidance strategy via virtual target approach[J]. Journal of Guidance, Control, and Dynamics, 2018, 41 (8): 1755- 1765.
doi: 10.2514/1.G003436 |
21 |
TEKIN R , ERER K S . Impact time and angle control against moving targets with look angle shaping[J]. Journal of Guidance, Control, and Dynamics, 2020, 43 (5): 1020- 1025.
doi: 10.2514/1.G004762 |
22 | 张友安, 梁勇, 刘京茂, 等. 基于轨迹成型的攻击角度与时间控制[J]. 航空学报, 2018, 39 (9): 143- 151. |
ZHANG Y A , LIANG Y , LIU J M , et al. Trajectory reshaping based impact angle and time control[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39 (9): 143- 151. | |
23 |
FERNANDEZ E C , SANZ L P , GARCIA J M C , et al. Conflict-free trajectory planning based on a data-driven conflict-resolution model[J]. Journal of Guidance, Control, and Dynamics, 2017, 40 (3): 615- 627.
doi: 10.2514/1.G000691 |
24 | SINGH V , WILLCOX K E . Methodology for path planning with dynamic data-driven flight capability estimation[J]. Journal of Guidance, Control, and Dynamics, 2017, 55 (8): 2727- 2738. |
25 |
IZZO D , OZTURK E . Real-time guidance for low-thrust transfers using deep neural networks[J]. Journal of Guidance, Control, and Dynamics, 2021, 44 (2): 315- 327.
doi: 10.2514/1.G005254 |
26 |
SANCHEZ C S , IZZO D . Real-time optimal control via deep neural networks: study on landing problems[J]. Journal of Guidance, Control, and Dynamics, 2018, 41 (5): 1122- 1135.
doi: 10.2514/1.G002357 |
27 | HE S , SHIN H S , TSOURDOS A . Computational missile guidance: a deep reinforcement learning approach[J]. Journal of Aerospace Information Systems, 2021, 18 (8): 571- 582. |
28 | 曾庆华, 董荣华, 皮术武. 基于最优制导模板的神经网络预测制导方法[J]. 国防科技大学学报, 2014, 36 (1): 137- 141. |
ZENG Q H , DONG R H , PI S W . Neural network predictive guidance method based on pattern of optimal guidance[J]. Journal of National University of Defense Technology, 2014, 36 (1): 137- 141. | |
29 | LI Q C , ZHANG W S , HAN G , et al. Finite time convergent wavelet neural network sliding mode control guidance law with impact angle constraint[J]. International Journal of Automation and Computing, 2015, 12 (6): 588- 599. |
30 | CHENG L , JIANG F H , WANG Z B , et al. Multiconstrained real-time entry guidance using deep neural networks[J]. IEEE Trans.on Aerospace and Electronic Systems, 2021, 57 (1): 325- 340. |
31 | GUO Y H , LI X , ZHANG H J , et al. Data-driven method for impact time control based on proportional navigation guidance[J]. Journal of Guidance, Control, and Dynamics, 2020, 43 (5): 955- 966. |
[1] | Mengping ZHOU, Xiuyun MENG, Junhui LIU. Design of optimal sliding mode guidance law for head-on interception of maneuvering targets with large angle of fall [J]. Systems Engineering and Electronics, 2022, 44(9): 2886-2893. |
[2] | Xiaohai WANG, Xiuyun MENG, Feng ZHOU, Wenjie QIU. Sliding mode guidance law with impact angle constraint based on bias proportional navigation [J]. Systems Engineering and Electronics, 2021, 43(5): 1295-1302. |
[3] | Chen MENG, Huahui YANG, Cheng WANG, Zheng MA. Review on data-driven fault diagnosis for electronic components and units level of weapon system [J]. Systems Engineering and Electronics, 2021, 43(2): 574-583. |
[4] | Liu YANG, Weigang ZHU, Shouye LYU, Shuang MA. Waveform unit extraction method for non-cooperative multi-function radar [J]. Systems Engineering and Electronics, 2021, 43(10): 2843-2850. |
[5] | JING Liang, ZHANG Zhongyang, CUI Naigang, WU Rong. Fixed time disturbance observer based terminal sliding mode guidance law [J]. Systems Engineering and Electronics, 2019, 41(8): 1820-1826. |
[6] | ZHANG Wenjie, LU Tianyu, XIA Qunli. Anti-early-warning airplane sliding mode guidance law based on extended state observer [J]. Systems Engineering and Electronics, 2019, 41(5): 1087-1093. |
[7] | WANG Tianning, TANG Shengjing, GUO Jie, ZHANG Yao. Biarc guidance law with terminal and dynamics constraints [J]. Systems Engineering and Electronics, 2019, 41(2): 372-381. |
[8] | JIANG Shang, TIAN Fuqing, SUN Shiyan, LIANG Weige, YOU Dong. Fuzzy adaptive dynamic surface terminal guidance law considering autopilot lag and impact angle constraints [J]. Systems Engineering and Electronics, 2019, 41(2): 389-401. |
[9] | WU Fang, CHANG Sijiang, CHEN Shengfu. Impact time control guidance law based on terminal sliding mode theory [J]. Systems Engineering and Electronics, 2019, 41(10): 2334-2342. |
[10] | LIU Bojun, HOU Mingshan, YU Ying. Guidance law with impact angle constraints based on immersion and invariance [J]. Systems Engineering and Electronics, 2018, 40(5): 1085-1090. |
[11] | WANG Xiaofang, CHAI Jin, ZHOU Jian. Cooperative path planning for multiple missiles based on piecewise Bezier curve [J]. Systems Engineering and Electronics, 2018, 40(10): 2317-2324. |
[12] | ZHANG Xiaojian, LIU Mingyong, LI Yang. Backstepping sliding mode control and extended state observer based guidance law design with impact angles [J]. Systems Engineering and Electronics, 2017, 39(6): 1311-1316. |
[13] | XU Jianguo, LI Mengjun, JIANG Jiang, YOU Hanlin. Data-driven motif analysis of technology breakthrough network [J]. Systems Engineering and Electronics, 2017, 39(5): 1072-1077. |
[14] | YANG Zhe, LIN De-fu, WANG Hui. Impact time control guidance law with field-of-view limit [J]. Systems Engineering and Electronics, 2016, 38(9): 2122-2128. |
[15] | WANG Guang-shuai, LIN De-fu, FAN Shi-peng, ZANG Lu-yao. Biased proportional navigation applicable for infrared guidance munitions [J]. Systems Engineering and Electronics, 2016, 38(10): 2346-2352. |
Viewed | ||||||
Full text |
|
|||||
Abstract |
|
|||||