In this paper, a novel cooperative guidance law is proposed to make multiple missiles in the
three-dimensional (3-D) space hit simultaneously the same target at pre-specified impact …

A three dimensional integrated guidance and control law with impact angle constraint is
developed, using the dynamic surface control and extended state observer techniques, for …

A novel impact angle constrained integrated guidance and control (IGC) scheme is
proposed with non-singular terminal sliding mode control (NTSMC) technique for missile to …

In this paper, a three-dimensional (3-D) distributed cooperative guidance scheme is
presented for multiple missiles to attack a single maneuvering target at pre-specified impact …

A partial integrated guidance and control design for an interception with terminal impact
angle constraints in three-dimensional space is presented in this paper. A three-dimensional …

Novel sliding-mode control laws are proposed in this paper to stabilize a class of uncertain
nonlinear systems. Considering that the sign function, which is often used in the sliding …

Considering a class of skid-to-turn (STT) missile with fixed target and constrained terminal
impact angles, a novel three-dimensional (3D) integrated guidance and control (IGC) …

In this paper, considering a class of skid-to-turn (STT) missile with impact angle constraint to
intercept the maneuvering target, a three-dimensional integrated guidance and control law …

ONE of the most popular guidance and control design paradigms that dominated the past
decades was the “separate” design principle (ie, designing the guidance law without …

This paper studies the integrated guidance and control (IGC) problem for a class of skid-to-
turn (STT) missiles subjected to rapidly changing actuator failures and coupled multisource …