Nonsingular terminal sliding mode guidance with impact angle constraints

SR Kumar, S Rao, D Ghose - Journal of Guidance, Control, and …, 2014 - arc.aiaa.org
Guidance laws based on a conventional sliding mode ensures only asymptotic
convergence. However, convergence to the desired impact angle within a finite time is …

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 …

Motion planning for multitarget surveillance with mobile sensor agents

Z Tang, U Ozguner - IEEE Transactions on Robotics, 2005 - ieeexplore.ieee.org
In the surveillance of multiple targets by mobile sensor agents (MSAs), system performance
relies greatly on the motion-control strategy of the MSAs. This paper investigates the motion …

Augmented polynomial guidance with impact time and angle constraints

TH Kim, CH Lee, IS Jeon… - IEEE Transactions on …, 2013 - ieeexplore.ieee.org
In this paper, a new impact time and impact angle control guidance law for homing missiles
against a stationary target is proposed. To derive a state feedback command for the …

Switched-gain guidance for impact angle control under physical constraints

R Tekin, KS Erer - Journal of Guidance, Control, and Dynamics, 2015 - arc.aiaa.org
The nonlinear impact angle control problem of a physically constrained pursuer against a
stationary ground target is solved through the use of a two-phased proportional navigation …

[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 …

Generalized vector explicit guidance

EJ Ohlmeyer, CA Phillips - Journal of guidance, control, and dynamics, 2006 - arc.aiaa.org
This paper proposes and evaluates a new guidance law termed generalized vector explicit
guidance (GENEX). This guidance law can simultaneously achieve design specifications on …

Impact time and angle control based on constrained optimal solutions

KS Erer, R Tekin - Journal of Guidance, Control, and Dynamics, 2016 - arc.aiaa.org
WHEN a pursuer for some reason modifies its otherwise direct course toward a target, two
key quantities that become significantly influenced are the impact time and the impact angle …