Attack Time Consensus Control for 3D Multi-Missile Systems Based on Adaptive Dynamic Programming

This investigation focuses on a collaborative control framework developed using a three-dimensional(3D) nonlinear guidance architecture. For the multi-missile system in 3D coordinate system, time-to-go and adaptive dynamic programming methods are used to control the motion of each missile simultaneously. In the Line-of-sight (LOS) coordinate system, the acceleration component along the LOS direction can make the attack time consensus of multi-missile system. The acceleration components in the direction of pitch Angle and deflection Angle are used for precise navigation. By leveraging adaptive dynamic programming (ADP), the proposed framework ensures synchronized attack timing across the multi-missile network while minimizing energy expenditure. The efficacy of the proposed approach is ultimately validated through computational modeling and simulation analysis.