2003•Electronics Optics & ControlRequires access
Derivation and simulation of a suboptimal midcourse guidance law for air-launched cruise missile
Feng Xing
Open publisher page 0 citations
Abstract
The attacking procedure of air launched cruise missile is introduced at first, then a mathematical model of midcourse guidance law is established and the optimal performance index is given. A new suboptimal midcourse guidance law is put forward based on primary theory of optimal control, and the result of simulation shows that the performance of missile is improved greatly.