Integrated missile guidance and control using optimization-based predictive control

摘要: This paper focuses on the design and implementation of optimization-based predictive control for problem missile interception. Due to inherent nonlinearities missile–target dynamics or even constraints, it is usually difficult a high-accuracy high-efficiency algorithm. A nonlinear receding horizon pseudospectral (RHPC) scheme constructed applied generate optimal command. The state estimation, in presence measurement noise, solved by implementing moving estimation (MHE) Since RHPC MHE algorithms solve online open-loop at each sampling instant, computational cost associated with them can be high. In order decrease demand due optimization process, recently proposed programming sensitivity-based algorithm used embedded framework. Numerical simulations analysis are presented demonstrate effectiveness scheme.