自适应非奇异快速终端二阶滑模制导律
Adaptive Nonsingular Fast Terminal Second-order Sliding Mode Guidance Law
查看参考文献18篇
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文摘
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针对打击机动目标带攻击角度约束的末制导问题,提出了一种带攻击角度约束的制导律。基于弹目相对运动模型,将攻击角度约束问题转化为终端视线角约束问题。设计了一种新型非奇异快速终端滑模面,结合改进的超螺旋算法,提出了一种自适应非奇异快速终端二阶滑模制导律。该制导律能够使弹目视线角及其角速率有限时间收敛,并设计了参数自适应律有效补偿未知扰动。通过仿真实验,验证了所提制导律能以期望攻击角度精确命中目标,且与现有制导律相比,收敛速度更快,制导精度更高,能量消耗更少。 |
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其他语种文摘
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Aiming at the terminal guidance with impact angle constraint against maneuvering targets,a guidance law with impact angle constraint was proposed. Based on the relative motion model of the missile and target,the impact angle constraint was transformed into the terminal line of sight(LOS)angle constraint. A new nonsingular fast terminal sliding-mode-surface was designed. Combined with the improved super-twisting algorithm,an adaptive nonsingular fast terminal second-order sliding-mode guidance law was proposed. The guidance law can make the LOS angle and LOS angular rate converge in finite-time,and a parameter adaptive-law was designed to effectively compensate the unknown disturbance. The simulation results indicate that by the proposed guidance law,the target can be accurately intercepted with expected impact angle. Compared with the existing guidance laws,the proposed guidance law has faster convergence speed,higher guidance precision and less energy consumption. |
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来源
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弹道学报
,2020,32(2):7-15 【核心库】
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DOI
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10.12115/j.issn.1004-499x(2020)02-002
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关键词
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制导律
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非奇异终端滑模
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有限时间收敛
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角度约束
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超螺旋算法
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二阶滑模
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地址
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1.
西安航空学院飞行器学院, 陕西, 西安, 710077
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洛阳电子信息装备试验中心, 河南, 洛阳, 471003
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语种
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中文 |
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文献类型
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研究性论文 |
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ISSN
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1004-499X |
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学科
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武器工业 |
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文献收藏号
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CSCD:6757706
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参考文献 共
18
共1页
|
|
1.
蔡洪. 具有终端角度约束的导引律综述.
宇航学报,2010,31(2):345-323
|
CSCD被引
1
次
|
|
|
|
|
2.
Song J M. Passive homing missile's variable structure proportional navigation with terminal angular constraint.
Chinese Journal of Aeronautics,2001,14(2):83-87
|
CSCD被引
18
次
|
|
|
|
|
3.
吴鹏. 带终端攻击角度约束的变结构制导律.
固体火箭技术,2008,31(2):116-120
|
CSCD被引
20
次
|
|
|
|
|
4.
Kumar S R. Sliding-mode guidance and control for all-aspect interceptors with terminal angle constraints.
Journal of Guidance,Control and Dynamics,2012,35(4):1230-1246
|
CSCD被引
61
次
|
|
|
|
|
5.
Song J H. Nonlinear disturbance observer based fast terminal sliding mode guidance with impact angle constraints.
International Journal of Innovative Computing,Information and Control,2015,11(3):787-802
|
CSCD被引
6
次
|
|
|
|
|
6.
Wang W H. Adaptive nonsingular terminal sliding mode guidance law against maneuvering targets with impact angle constraint.
Proceedings of the Institution of Mechanical Engineers,Part G:Journal of Aerospace Engineering,2015,229(5):867-890
|
CSCD被引
4
次
|
|
|
|
|
7.
Song J H. Three-dimensional guidance law based on adaptive integral sliding mode control.
Chinese Journal of Aeronautics,2016,29(1):202-214
|
CSCD被引
23
次
|
|
|
|
|
8.
熊少锋. 带攻击角度约束的非奇异快速终端滑模制导律.
控制理论与应用,2014,31(3):269-278
|
CSCD被引
32
次
|
|
|
|
|
9.
Zhang Z L. Strictly convergent non-singular terminal sliding mode guidance law with impact angle constraints.
Optik,2016,127(22):10971-10980
|
CSCD被引
5
次
|
|
|
|
|
10.
Zhang N. A fast finite-time convergent guidance law with nonlinear disturbance observer for unmanned aerial vehicles collision avoidance.
Aerospace Science and Technology,2019,86:204-214
|
CSCD被引
8
次
|
|
|
|
|
11.
Song J H. Robust impact angel constraints guidance law with autopilot lag and acceleration saturation consideration.
Transactions of the Institute of Measurement and Control,2019,41(1):182-192
|
CSCD被引
2
次
|
|
|
|
|
12.
Levant A. Principles of 2-sliding mode design.
Automatica,2007,43(4):576-586
|
CSCD被引
73
次
|
|
|
|
|
13.
He S M. Continuous second-order sliding mode based impact angle guidance law.
Aerospace Science and Technology,2015,41:199-208
|
CSCD被引
12
次
|
|
|
|
|
14.
Zhou A M. Finite-time output feedback attitude tracking control for rigid spacecraft.
IEEE Transactions on Control Systems Technology,2014,22(1):338-345
|
CSCD被引
14
次
|
|
|
|
|
15.
Li B. Observer-based fault-tolerant attitude control for rigid spacecraft.
IEEE Transactions on Aerospace and Electronic Systems,2017,53(5):2572-2582
|
CSCD被引
15
次
|
|
|
|
|
16.
Li H. On SFTSM control with fixed-time convergence.
IET Control Theory & Applications,2017,11(6):766-773
|
CSCD被引
18
次
|
|
|
|
|
17.
Evangelista C. Lyapunov-designed super-twisting sliding mode control for wind energy conversion optimization.
IEEE Transactions on Industrial Electronics,2013,60(2):538-545
|
CSCD被引
11
次
|
|
|
|
|
18.
Cong B L. On adaptive sliding mode control without switching gain overestimation.
International Journal of Robust and Nonlinear Control,2014,24(3):515-531
|
CSCD被引
6
次
|
|
|
|
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