Acta Aeronautica et Astronautica Sinica ›› 2023, Vol. 44 ›› Issue (15): 528764-528764.doi: 10.7527/S1000-6893.2023.28764
• Flight Mechanics and Guidance Control • Previous Articles Next Articles
Haojian LI1,2, Yuanhe LIU1,2, Yangang LIANG1,2, Kebo LI1,2()
Received:
2023-03-30
Revised:
2023-04-24
Accepted:
2023-05-15
Online:
2023-08-15
Published:
2023-05-17
Contact:
Kebo LI
E-mail:likeboreal@nudt.edu.cn
Supported by:
CLC Number:
Haojian LI, Yuanhe LIU, Yangang LIANG, Kebo LI. Prescribed performance guidance law with field-of-view and impact angle constraints[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528764-528764.
1 | KIM M, GRIDER K. Terminal guidance for impact attitude angle constrained flight trajectories[J]. IEEE Transactions on Aerospace and Electronic Systems, 1973, AES-9(6): 852-859. |
2 | RYOO C K, TAHK M J. Time-to-go weighted optimal guidance with impact angle constraints[J]. IEEE Transactions on Control Systems Technology, 2006, 14(3): 483-492. |
3 | LI R, WEN Q Q, TAN W C. Adaptive weighting impact angle optimal guidance law considering seeker’s FOV angle constraints[J]. Journal of Systems Engineering and Electronics, 2018, 29(1): 142-151. |
4 | KIM J, CHO S. Optimal guidance law for impact angle and acceleration constraints with time-varying gains[J]. International Journal of Aeronautical and Space Sciences, 2022, 23(3): 609-621. |
5 | KUMAR S R, RAO S, GHOSE D. Sliding-mode guidance and control for all-aspect interceptors with terminal angle constraints[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(4): 1230-1246. |
6 | BISWAS B, KUMAR S R, MAITY A. Three-dimensional nonlinear impact angle guidance for maneuvering targets[J]. IFAC-PapersOnLine, 2018, 51(1): 47-52. |
7 | KIM H G, KIM H J. All-aspect guidance with impact angle constraint against unknown target maneuver[J]. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55(2): 830-845. |
8 | ZHOU Z M, YAO X X. Polynomial guidance law for impact angle control with a seeker look angle limit[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, 234(3): 857-870. |
9 | HU Q L, CAO R H, HAN T, et al. Field-of-view limited guidance with impact angle constraint and feasibility analysis[J]. Aerospace Science and Technology, 2021, 114: 106753. |
10 | FU S N, ZHOU G Q, XIA Q L. A trajectory shaping guidance law with field-of-view angle constraint and terminal limits[J]. Journal of Systems Engineering and Electronics, 2022, 33(2): 426-437. |
11 | 黎克波, 廖选平, 梁彦刚, 等. 基于纯比例导引的拦截碰撞角约束制导策略[J]. 航空学报, 2020, 41(S2): 724277. |
LI K B, LIAO X P, LIANG Y G, et al. Guidance strategy with impact angle constraint based on pure proportional navigation[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(S2): 724277 (in Chinese). | |
12 | SHIN H S, Li K B. An improvement in three-dimensional pure proportional navigation guidance[J]. IEEE Transactions on Aerospace and Electronic Systems, 2021, 57(5): 3004-3014. |
13 | LI K B, SHIN H S, TSOURDOS A, et al. Performance of 3-D PPN against arbitrarily maneuvering target for homing phase[J]. IEEE Transactions on Aerospace and Electronic Systems, 2020, 56(5): 3878-3891. |
14 | LI K B, SHIN H S, TSOURDOS A, et al. Capturability of 3D PPN against lower-speed maneuvering target for homing phase[J]. IEEE Transactions on Aerospace and Electronic Systems, 2020, 56(1): 711-722. |
15 | KIM B S, LEE J G, HAN H S. Biased PNG law for impact with angular constraint[J]. IEEE Transactions on Aerospace and Electronic Systems, 1998, 34(1): 277-288. |
16 | ERER K S, MERTTOPÇUOĜLU O. Indirect impact-angle-control against stationary targets using biased pure proportional navigation[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(2): 700-704. |
17 | KIM T H, PARK B G, TAHK M J. Bias-shaping method for biased proportional navigation with terminal-angle constraint[J]. Journal of Guidance, Control, and Dynamics, 2013, 36(6): 1810-1816. |
18 | 闫梁, 赵继广, 沈怀荣, 等. 带末端碰撞角约束的三维联合偏置比例制导律设计[J]. 航空学报, 2014, 35(7): 1999-2010. |
YAN L, ZHAO J G, SHEN H R, et al. Three-dimensional united biased proportional navigation guidance law for interception of targets with angular constraints [J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(7): 1999-2010 (in Chinese). | |
19 | XU X Y, LIANG Y. Biased optimal guidance law with specified velocity rendezvous angle constraint[J]. The Aeronautical Journal, 2015, 119(1220): 1287-1299. |
20 | LEE C H, KIM T H, TAHK M J. Interception angle control guidance using proportional navigation with error feedback[J]. Journal of Guidance, Control, and Dynamics, 2013, 36(5): 1556-1561. |
21 | HE S M, LEE C H. Optimality of error dynamics in missile guidance problems[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(7): 1624-1633. |
22 | 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): 322215. |
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): 322215 (in Chinese). | |
23 | 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. |
24 | WANG C Y, DONG W, WANG J N, et al. Guidance law design with fixed-time convergent error dynamics[J]. Journal of Guidance, Control, and Dynamics, 2021, 44(7): 1389-1398. |
25 | CHENG Z T, WU H, WANG B, et al. Fixed-time convergent guidance law with impact angle control[J]. Complexity, 2020, 2020: 1-9. |
26 | SONG Y D, WANG Y J, HOLLOWAY J, et al. Time-varying feedback for regulation of normal-form nonlinear systems in prescribed finite time[J]. Automatica, 2017, 83: 243-251. |
27 | PAL A K, KAMAL S, NAGAR S K, et al. Design of controllers with arbitrary convergence time[J]. Automatica, 2020, 112: 108710. |
28 | BECHLIOULIS C P, ROVITHAKI G A. Adaptive control with guaranteed transient and steady state tracking error bounds for strict feedback systems[J]. Automatica, 2009, 45(2): 532-538. |
29 | LI X, YE J K, ZHOU C J, et al. Prescribed performance guidance law with multiple constraints[J]. International Journal of Aerospace Engineering, 2022, 2022: 1-17. |
30 | LYU S, YAN X D, TANG S. Prescribed performance interceptor guidance with terminal line of sight angle constraint accounting for missile autopilot lag[J]. Aerospace Science and Technology, 2017, 69: 171-180. |
31 | LYU S, ZHU Z H, TANG S, et al. Prescribed performance slide mode guidance law with terminal line-of-sight angle constraint against maneuvering targets[J]. Nonlinear Dynamics, 2017, 88(3): 2101-2110. |
32 | BU X W, QI Q, JIANG B X. A Simplified finite-time fuzzy neural controller with prescribed performance applied to waverider aircraft[J]. IEEE Transactions on Fuzzy Systems, 2022, 30(7): 2529-2537. |
33 | 李旭, 叶继坤, 邵雷, 等. 基于有限时间小超调预设性能控制的三维滑模末制导律设计[J]. 航空兵器,2022 (in press). |
LI X, YE J K, SHAO L, et al. Design of three dimensional sliding mode terminal guidance law based on finite-time and small-overshoot prescribed performance control[J]. Aero Weaponry, 2022 (in press) (in Chinese). | |
34 | HE S M, LEE C H, SHIN H S, et al. Optimal guidance and its applications in missiles and UAVs[M]. Cham: Springer International Publishing, 2020: 54-58. |
35 | ZHANG W J, FU S N, LI W, et al. An impact angle constraint integral sliding mode guidance law for maneuvering targets interception[J]. Journal of Systems Engineering and Electronics, 2020,31(1): 168-184. |
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Total visits: 6658907 Today visits: 1341