TY - GEN
T1 - Distributed group cooperative guidance for multiple missiles with switching directed communication topologies
AU - Zhao, Qilun
AU - Dong, Xiwang
AU - Liang, Zixuan
AU - Ren, Zhang
N1 - Publisher Copyright:
© 2017 Technical Committee on Control Theory, CAA.
PY - 2017/9/7
Y1 - 2017/9/7
N2 - Distributed group cooperative guidance (DGCG) problems for multiple missiles with switching directed communication topologies are dealt with. In contrast to traditional cooperative guidance utilized to intercept one single target, the group cooperative guidance is applicable to multiple targets. In the group cooperative attack, multi-missile system are classified into multiple subgroups, and each subgroup attacks its respective target. Missiles in the same subgroup are required to reach the target simultaneously, while different subgroups may cooperate successively in terms of the impact time. To realize the group cooperative attack, a two-step guidance strategy is developed. The first step adopts a DGCG law based on local neighboring information for multiple missiles to realize group consensus on range-to-go and leading angle. The second step begins when the group consensus of missiles is achieved. During this step, each missile attacks the target under the proportional navigation (PN) guidance law. Derived from a feedback linearization approach and convergence analysis, sufficient conditions for multiple missiles to realize the group cooperative attack with switching directed communication topologies are proposed, respectively. Finally, numerical examples are given to show the effectiveness of the two-step guidance strategy.
AB - Distributed group cooperative guidance (DGCG) problems for multiple missiles with switching directed communication topologies are dealt with. In contrast to traditional cooperative guidance utilized to intercept one single target, the group cooperative guidance is applicable to multiple targets. In the group cooperative attack, multi-missile system are classified into multiple subgroups, and each subgroup attacks its respective target. Missiles in the same subgroup are required to reach the target simultaneously, while different subgroups may cooperate successively in terms of the impact time. To realize the group cooperative attack, a two-step guidance strategy is developed. The first step adopts a DGCG law based on local neighboring information for multiple missiles to realize group consensus on range-to-go and leading angle. The second step begins when the group consensus of missiles is achieved. During this step, each missile attacks the target under the proportional navigation (PN) guidance law. Derived from a feedback linearization approach and convergence analysis, sufficient conditions for multiple missiles to realize the group cooperative attack with switching directed communication topologies are proposed, respectively. Finally, numerical examples are given to show the effectiveness of the two-step guidance strategy.
KW - Missile guidance
KW - cooperative guidance
KW - group consensus
KW - multiple missiles
KW - switching communication topologies
UR - http://www.scopus.com/inward/record.url?scp=85032183834&partnerID=8YFLogxK
U2 - 10.23919/ChiCC.2017.8028268
DO - 10.23919/ChiCC.2017.8028268
M3 - Conference contribution
AN - SCOPUS:85032183834
T3 - Chinese Control Conference, CCC
SP - 5741
EP - 5746
BT - Proceedings of the 36th Chinese Control Conference, CCC 2017
A2 - Liu, Tao
A2 - Zhao, Qianchuan
PB - IEEE Computer Society
T2 - 36th Chinese Control Conference, CCC 2017
Y2 - 26 July 2017 through 28 July 2017
ER -