In this paper, a new continuous robust impact angle constraint guidance law with finite-time
convergence is proposed for intercepting maneuvering targets with unknown acceleration …

In this paper, the terminal guidance problem of unpowered lifting reentry vehicle to
stationary target is studied. Based on the requirement of attacking the target with high …

This study explores the guidance law against maneuvering targets with the intercept angle
constraint. The limitation of the traditional guidance law, which simply treats the unknown …

To concretely provide a feasible solution for homing missiles with the precise impact time
and angle, this paper develops a novel guidance law, based on the nonlinear engagement …

To steer a hypersonic vehicle of high Lift-to-Drag ratio (L/D) safely and accurately, a new
entry guidance is proposed based on drag-vs-energy profile. Over the rotating Earth, by …

This paper is denoted to investigating stability in mean of partial variables for stochastic
reaction–diffusion equations with Markovian switching (SRDEMS). By transforming the …

In this paper, the problem of 3-dimensional guidance law design is considered and a new
guidance law based on partial sliding mode technique is presented. The approach is based …

This paper has proposed two continuous composite finite-time convergent guidance laws to
intercept maneuvering targets in the presence of autopilot lag: one is for hit-to-kill and the …

In this paper, three dimensional coupled engagement dynamics are firstly transformed into a
state‐space form without decoupling three dimensional engagement dynamics into two …

This paper presents a novel technique to design a robust finite-time partial stabilizer, based
on the non-singular terminal sliding mode method and a disturbance observer for the missile …