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.
In real applications, the moving targets usually include both maneuvering and non-maneuvering situations.
Whilst this paper mainly focuses on state estimation and data fusion for unknown non-linear dynamic processes, maneuvering targets are also briefly considered.
A prescribed performance guidance law during the terminal homing phase is proposed to intercept a non-cooperative maneuvering target in this paper.
A coordinated turn case study of maneuvering target in the presence of non-Gaussian noise is of particular interest.
Considering the characteristics of non-stationary target signals, joint estimation of DOD and DOA information of maneuvering targets was examined in [11] exploiting spatial time-frequency distribution.
A dynamic differential correction algorithm is presented to deliver an impulsive maneuver to a satellite to place it within overlapping spheres, with user defined radii, centered around multiple non-maneuvering satellites and ground location׳s user defined line-of-sight within a constrained time.
Only seven studies were eligible for inclusion in the meta-analysis of non-VC maneuver, as opposed to 12 studies for the VC maneuver, and the low 95 % CI limit of the former may be due to the limited sample size.
It is assumed that a single non-maneuvering target is in the presence of clutter.
Scenario 1: Two constant-speed, non-maneuvering targets whose paths cross.
Missile defense systems, using conventional guidance, demonstrated hit-to-kill accuracy against non-maneuvering targets.
