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An Optimal Geometrical Guidance Law for Impact Time and Angle Control

IEEE Transactions on Aerospace and Electronic Systems, 2023
This article proposes an impact time and angle control guidance law based on geometry without estimating the time-to-go. A moving virtual target is artificially placed on the desired collision line, and the missile pursues the virtual target to satisfy ...
Libing Hou   +4 more
semanticscholar   +1 more source

Fixed-Time Terminal Angle-Constrained Cooperative Guidance Law Against Maneuvering Target

IEEE Transactions on Aerospace and Electronic Systems, 2021
In this article, fixed-time cooperative guidance laws are designed for multiple missiles to simultaneously attack a maneuvering target at desired terminal angles.
Wei Dong   +4 more
semanticscholar   +1 more source

Three-Dimensional Impact Angle and Time Control Guidance Law Based on Two-Stage Strategy

IEEE Transactions on Aerospace and Electronic Systems, 2022
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 angle control guidance (IACG) and proportional navigation guidance (PNG ...
Chunyan Wang   +3 more
semanticscholar   +1 more source

Prescribed-time cooperative guidance law against manoeuvring target with input saturation

International Journal of Control, 2022
This paper proposes a novel prescribed-time cooperative guidance law (PTCGL) for multiple missiles cooperatively attacking a manoeuvring target. Guidance models in two directions are used and the acceleration saturations are also considered in both two ...
Zhikai Wang   +4 more
semanticscholar   +1 more source

Cooperative guidance law for multiple missiles simultaneous attacks with fixed-time convergence

International Journal of Control, 2022
This paper considers the problem of multiple missiles to attack a maneuvering target simultaneously. Based on a fixed-time fast nonsingular terminal sliding mode surface (FNTSMS), fixed-time distributed cooperative guidance laws are developed.
Hang Yu   +6 more
semanticscholar   +1 more source

Three-dimensional cooperative guidance law to control impact time and angle with fixed-time convergence

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2022
This article proposes a new terminal cooperative guidance law to control both impact time and impact angle in three-dimensional engagement. The presented guidance law employs on and normal line-of-sight accelerations to control the impact time and angle ...
Hong-Xia Li, Huijie Li, Yuan-li Cai
semanticscholar   +1 more source

Design of Line-of-Sight Guidance Law and a Constrained Optimal Controller for an Autonomous Underwater Vehicle

IEEE Transactions on Circuits and Systems - II - Express Briefs, 2021
A line-of-sight (LOS) guidance law with an explicit model predictive control (MPC) is proposed for an underactuated autonomous underwater vehicle (AUV). The derived LOS law is based on quaternion angles thus avoids the problem of singularity inherited in
R. Rout, B. Subudhi
semanticscholar   +1 more source

Three-Dimensional Nonsingular Cooperative Guidance Law with Different Field-of-View Constraints

Journal of Guidance Control and Dynamics, 2021
In this paper, a distributed three-dimensional (3D) nonsingular cooperative guidance law is designed for multiple missiles with different seeker’s field-of-view (FOV) constraints to achieve salvo a...
Wei Dong   +3 more
semanticscholar   +1 more source

Quaternion Based Three-Dimensional Impact Angle Control Guidance Law

IEEE Transactions on Aerospace and Electronic Systems, 2021
This article deals with a guidance law for impact angle control (IAC) in the 3-D space. Extended from the 2-D IAC law, the proposed guidance law is derived using a quaternion.
Jeong-Hun Kim   +3 more
semanticscholar   +1 more source

State Estimation With a Destination Constraint Imposed by Proportional Navigation Guidance Law

IEEE Transactions on Aerospace and Electronic Systems, 2021
Proportional navigation (PN) guidance laws have been commonly applied to homing missile systems guiding the missile to its target. When the target is stationary and its location is known a priori, the state of the missile is subjected to a destination ...
Keyi Li, Gongjian Zhou
semanticscholar   +1 more source

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