Fixed-time terminal angle-constrained cooperative guidance law against maneuvering target
In this article, fixed-time cooperative guidance laws are designed for multiple missiles to
simultaneously attack a maneuvering target at desired terminal angles. The 3-D guidance …
simultaneously attack a maneuvering target at desired terminal angles. The 3-D guidance …
Impact-angle-constrained cooperative guidance for salvo attack
This paper proposes distributed cooperative guidance laws for multiple missiles with
constant speeds to achieve impact-angle-constrained salvo attack against a stationary target …
constant speeds to achieve impact-angle-constrained salvo attack against a stationary target …
Guidance law design with fixed-time convergent error dynamics
FOR decades, the proportional navigation guidance (PNG) law has been widely applied in
various guidance problems due to its implementation simplicity and efficiency [1]. The PNG …
various guidance problems due to its implementation simplicity and efficiency [1]. The PNG …
Three-dimensional vector guidance law with impact time and angle constraints
Abstract The three-dimensional (3D) impact time and angle guidance problem is of great
practical significance but remains open because of the coupling nonlinearity and multiple …
practical significance but remains open because of the coupling nonlinearity and multiple …
Unified method for field-of-view-limited homing guidance
Homing guidance requires maintaining the target lock-on condition within the seeker's field
of view (FOV). This paper aims at developing a unified FOV-limited guidance framework …
of view (FOV). This paper aims at developing a unified FOV-limited guidance framework …
Nonlinear three-dimensional guidance for impact time and angle control with field-of-view constraint
This article presents a nonlinear 3-D guidance law for homing missiles with a field-of-view
(FOV) constraint to achieve impact time and angle control against a stationary target …
(FOV) constraint to achieve impact time and angle control against a stationary target …
Three-dimensional impact angle and time control guidance law based on two-stage strategy
In this article, a 3-D nonlinear guidance law is developed for attacking a stationary target
with desired impact angle and time. The guidance law is divided into two stages—impact …
with desired impact angle and time. The guidance law is divided into two stages—impact …
A novel controller for nonlinear uncertain systems using a combination of SDRE and function approximation technique: Regulation and tracking of flexible-joint …
This paper presents a novel combined State Dependent Riccati Equation (SDRE)/Function
Approximation Technique (FAT)-based control design for nonlinear uncertain systems. The …
Approximation Technique (FAT)-based control design for nonlinear uncertain systems. The …
Impact time and angle control optimal guidance with field-of-view constraint
Y Chen, S Wu, X Wang - Journal of Guidance, Control, and Dynamics, 2022 - arc.aiaa.org
TRADITIONAL guidance laws like classical proportional navi-gation guidance (PNG) usually
only focus on zero miss distance. However, with the rapid growth of modern defense system …
only focus on zero miss distance. However, with the rapid growth of modern defense system …
Field-of-view constrained three-dimensional impact angle control guidance for speed-varying missiles
This article develops a three-dimensional (3-D) impact angle control guidance law with the
field-of-view (FOV) constraint. The impact error is defined as the difference between the …
field-of-view (FOV) constraint. The impact error is defined as the difference between the …