Event-based optimal guidance laws design for missile-target interception systems using fuzzy dynamic programming approach

Abstract In this paper, the guidance system with unknown dynamics is modeled as a partially unknown zero-sum differential game system. Then, a periodic event-triggered optimal control algorithm is designed to interception target under a plug-n-play framework. To realize this algorithm, generalized fuzzy hyperbolic models are employed to construct the identifier-critic structure, where the online identifier is used to estimate unknown dynamics, meanwhile, the generalized fuzzy hyperbolic models-based critic network is utilized to approximate the cost function. Note that plug-n-play framework lets both the designed identifier and critic network work simultaneously, in other words, the prior system information is no longer required, which simplifies the network structure. Using the Lyapunov function method, the approximate optimal control strategy and corresponding weight updating laws are derived to guarantee that the closed-loop system and weight approximation errors are uniformly ultimately bounded, where an additional function is added to weight updating laws to release the requirement for admissible initial control. Finally, to compare the intercept effects and the utilization ratio of communication resources of the periodic event-triggered control algorithm and the common adaptive dynamic programming algorithm, the missile interception system is introduced as an example.