In this paper, sliding mode control-based impact time guidance laws are proposed. Even for
large heading angle errors and negative initial closing speeds, the desired impact time is …

This paper investigates the problem of impact-angle-constrained guidance law design
against maneuvering target with large initial heading error. The guidance problem is first …

Fixed-wing unmanned aerial vehicles (UAVs) can be an essential tool for low-cost aerial
surveillance and map** applications in remote regions. There is, however, a key …

This paper presents an impact angle control guidance law that confines the missile look
angle during homing in order to not exceed a seeker's field-of-view limit. A sliding surface …

A new generalized model predictive static programming technique is presented for rapidly
solving a class of finite-horizon nonlinear optimal control problems with hard terminal …

In this article, a guidance law with impact angle constraint is developed using the state-
dependent Riccati equation (SDRE) technique. First, the nonlinear guidance dynamics …

This article presents a new 3-D nonlinear optimal guidance law to control the impact angle
in maneuvering target interception. This approach formulates the optimization problem in a …

The problem of impact angle control guidance for a field-of-view constrained missile against
non-maneuvering or maneuvering targets is solved by using the sliding mode control theory …

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 …

For the problem of intercepting a maneuvering target with a desired terminal impact angle,
we propose a guidance law in this article based on a nonlinear relative virtual guidance …