Impact-time-control guidance law for anti-ship missiles

IS Jeon, JI Lee, MJ Tahk - IEEE Transactions on control …, 2006 - ieeexplore.ieee.org
In this paper, a new guidance problem with the impact time constraint is investigated, which
can be applied to salvo attack of anti-ship missiles. The closed form solution based on the …

Impact time and angle guidance with sliding mode control

N Harl, SN Balakrishnan - IEEE Transactions on control …, 2011 - ieeexplore.ieee.org
A novel sliding mode-based impact time and angle guidance law for engaging a modern
warfare ship is presented in this paper. In order to satisfy the impact time and angle …

Sliding-mode guidance and control for all-aspect interceptors with terminal angle constraints

SR Kumar, S Rao, D Ghose - Journal of Guidance, Control, and …, 2012 - arc.aiaa.org
THE main objective of guided missiles is to intercept targets with minimum miss distances
while optimizing the energy usage to increase their range. Current applications demand …

Guidance law to control impact time and angle

JI Lee, IS Jeon, MJ Tahk - IEEE Transactions on Aerospace …, 2007 - ieeexplore.ieee.org
This paper proposes a new guidance law to control both impact time and impact angle for a
flight vehicle's homing problem, which can be applied for an efficient salvo attack of antiship …

Time-to-go weighted optimal guidance with impact angle constraints

CK Ryoo, H Cho, MJ Tahk - IEEE Transactions on control …, 2006 - ieeexplore.ieee.org
In this paper, the optimal guidance law with terminal constraints of miss distance and impact
angle is presented for a constant speed missile against the stationary target. The proposed …

Linear quadratic guidance laws for imposing a terminal intercept angle

V Shaferman, T Shima - Journal of Guidance, Control, and Dynamics, 2008 - arc.aiaa.org
Linear quadratic guidance laws that explicitly enable imposing a predetermined intercept
angle are presented. Two such guidance laws are derived, using optimal control and …

[HTML][HTML] Guidance law with impact time and impact angle constraints

Y Zhang, G Ma, A Liu - Chinese Journal of Aeronautics, 2013 - Elsevier
A novel closed-form guidance law with impact time and impact angle constraints is proposed
for salvo attack of anti-ship missiles, which employs missile's normal acceleration (not jerk) …

Polynomial guidance laws considering terminal impact angle and acceleration constraints

CH Lee, TH Kim, MJ Tahk… - IEEE Transactions on …, 2013 - ieeexplore.ieee.org
The work presented here investigates proposed impact angle control guidance laws with
terminal acceleration constraints for a stationary or slowly moving target. These laws, called …

Cooperative optimal guidance laws for imposing a relative intercept angle

V Shaferman, T Shima - Journal of Guidance, Control, and Dynamics, 2015 - arc.aiaa.org
Optimal control-based cooperative guidance laws, which enforce at intercept a relative
geometry in between a group of missiles and a single maneuvering target, are presented …

Cooperative differential games guidance laws for imposing a relative intercept angle

V Shaferman, T Shima - Journal of Guidance, Control, and Dynamics, 2017 - arc.aiaa.org
A cooperative guidance law for a team of interceptors trying to intercept, from multiple
directions, an evading target is proposed. An example scenario of interest is that of …