摘要
To eliminate the perturbation of interceptor detection induced by aerodynamic heating,the head pursuit (HP) guidance law for three-dimensional interception was presented. The guidance law positioned the interceptor ahead of the target on its flight trajectory,and the speed of interceptor was required to be lower than that of the target. On the basis of a novel head pursuit three-dimensional guidance model,a nonlinear guidance law was developed based on smooth sliding mode control theory. At the same time,a special observer was designed to estimate the target acceleration,and a numerical example on maneuvering ballistic target interception verified the effectiveness of the presented guidance law.
To eliminate the perturbation of interceptor detection induced by aerodynamic heating, the head pursuit （HP） guidance law for three-dimensional interception was presented. The guidance law positioned the interceptor ahead of the target on its flight trajectory, and the speed of interceptor was required to be lower than that of the target. On the basis of a novel head pursuit three-dimensional guidance model, a nonlinear guidance law was developed based on smooth sliding mode control theory. At the same time, a special observer was designed to estimate the target acceleration, and a numerical example on maneuvering ballistic target interception verified the effectiveness of the presented guidance law.
