Abstract: A guidance law with finite time convergence is designed using the sliding mode control method and finite time convergence control theory, accounting for the missile autopilot as secondorder dynamics. The highorder derivatives ...

Abstract: A slidingmode guidance (SMG) law is designed to intercept maneuvering targets with impact angle constrained flight trajectories under the assumption of ideal missile autopilot. Furthermore, accounting for the autopilot as ...

Abstract: The line-of-sight (LOS) kinematics and dynamics of a mirror-stabilized platform are derived using the virtual mass stabilization method. Accounting for the coupled and nonlinear kinematics and dynamics, the uncertainty of ...

Abstract: Based on the discrete form of the targetmissile relative motion equations in plane, a discrete slidingmode guidance (DSMG) law is proposed. All previous missile seeker's measurements are used in the design of the DSMG law ...

Abstract: This paper addresses a pursuer tracking problem where the pursuer's acceleration is given by a proportional navigation (PN) guidance law with a time-varying navigation ratio which varies with the relative range between the ...