Sep 5, 2017 � In this paper, a novel approximate finite-time convergent guidance law for missiles is presented to accurately intercept maneuvering targets�...
In this paper, a novel approximate finite-time convergent guidance law for missiles is presented to accurately intercept maneuvering targets when the�...
Dive into the research topics of 'A novel approximate finite-time convergent guidance law with actuator fault'. Together they form a unique fingerprint. Sort by�...
In this paper, a novel approximate finite-time convergent guidance law for missiles is presented to accurately intercept maneuvering targets when the�...
This paper aims to develop hit-to-kill guidance laws for missile interception with actuator faults. New fault- tolerant control schemes with sliding mode�...
Sep 21, 2018 � This paper aims to develop a new finite-time convergent guidance law for intercepting maneuvering targets accounting for second-order autopilot lag.
Apr 28, 2023 � In this paper, a new fixed-time convergence guidance law is proposed against maneuvering targets in the three-dimensional (3-D) engagement scenario.
Missing: fault. | Show results with:fault.
A finite-time impact angle control guidance law is developed using the fast nonsingular terminal sliding mode control theory.
Missing: fault. | Show results with:fault.
A novel approximate finite-time convergent guidance law with actuator fault � Wei WangYi JiD. LinZhongjiao ShiShiyao Lin. Engineering. Cluster Computing. 2017.
Nov 13, 2023 � In this paper, a prescribed-time guidance law with approach angle constraint in the presence of an actuator fault is proposed.