Three-dimensional finite-time cooperative guidance for multiple missiles without radial velocity measurements

被引:47
作者
Lyu, Teng [1 ]
Li, Chuanjiang [1 ]
Guo, Yanning [1 ]
Ma, Guangfu [1 ]
机构
[1] Harbin Inst Technol, Dept Control Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China
基金
中国国家自然科学基金;
关键词
3-D cooperative guidance; Directed communication topologies; Finite time; Impact angle constraint; Radial velocity measurements; 2ND-ORDER MULTIAGENT SYSTEMS; FORMATION-CONTAINMENT CONTROL; EULER-LAGRANGE SYSTEMS; CONSENSUS; LAW; TRACKING; IMPACT; ATTACK; STABILIZATION; STABILITY;
D O I
10.1016/j.cja.2018.12.005
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In order to simultaneously attack a target with impact angle constraint in three-dimensional (3-D) space, a novel distributed cooperative guidance law for multiple missiles under directed communication topologies is proposed without radial velocity measurements. First, based on missiles-target 3-D relative motion equations, the multiple missiles cooperative guidance model with impact angle constraint is constructed. Then, in Line-of-Sight (LOS) direction, based on multi-agent system cooperative control theory, one guidance law with directed topologies is designed with strict proof, which can guarantee finite time consensus of multiple missiles' impact times. Next, in elevation direction and azimuth direction of LOS, based on homogeneous system stability theory and integral sliding mode control theory, two guidance laws are proposed respectively with strict proof, which can guarantee LOS angles converge to desired values and LOS angular rates converge to zero in finite time. Finally, the effectiveness of the designed cooperative guidance law is demonstrated through simulation results. (C) 2019 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.
引用
收藏
页码:1294 / 1304
页数:11
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