AbstractA projectile is analyzed which uses a bang-bang type guidance law with a wind stabilized seeker. The projectile is guided to a target located on the ground. The projectile motion is modelled in the vertical plane, and the model is used to compare the performance of the wind stabilized seeker system with that of proportional navigation. The effects of wind speed and target motion on guidance accuracy are analyzed. Finally the results are compared to results obtained from a full 6 degrees of freedom simulation of the system
The purpose of guidance is to cause a collision between a missile and a specified target. Accordingl...
In this study, it is aimed at comparing the performance of the guidance methods called Linear Homing...
Abstract — A missile system employed with homing guidance can sense and detect the target, guide its...
AbstractA projectile is analyzed which uses a bang-bang type guidance law with a wind stabilized see...
AbstractA projectile which uses a bang-bang type guidance law is launched, and its goal is to hit a ...
AbstractA projectile which uses a bang-bang type guidance law is launched and its goal is to hit a f...
AbstractA projectile which uses a bang-bang type guidance law is considered. Two problems concerning...
The paper briefly reviews the guidance laws and their implementation in surface-to-airmissiles. The ...
This paper considers the problem of mimicking short-range ballistic trajectories and presents a feed...
This dissertation studies the optimal guidance of homing missiles. The guidance objective is to dete...
A defense system against ballistic threat is a very complex system from the engineering point of vie...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76681/1/AIAA-1988-4066-823.pd
This paper will talk about AIM 120 AMRAAM missile guidance for pursuing a moving target. The missile...
A new suboptimal guidance law is presented. It uses proportional navigation with phase lead compensa...
The efficacy of a munition depends on target detection, estimation of its motion, guidance, tracking...
The purpose of guidance is to cause a collision between a missile and a specified target. Accordingl...
In this study, it is aimed at comparing the performance of the guidance methods called Linear Homing...
Abstract — A missile system employed with homing guidance can sense and detect the target, guide its...
AbstractA projectile is analyzed which uses a bang-bang type guidance law with a wind stabilized see...
AbstractA projectile which uses a bang-bang type guidance law is launched, and its goal is to hit a ...
AbstractA projectile which uses a bang-bang type guidance law is launched and its goal is to hit a f...
AbstractA projectile which uses a bang-bang type guidance law is considered. Two problems concerning...
The paper briefly reviews the guidance laws and their implementation in surface-to-airmissiles. The ...
This paper considers the problem of mimicking short-range ballistic trajectories and presents a feed...
This dissertation studies the optimal guidance of homing missiles. The guidance objective is to dete...
A defense system against ballistic threat is a very complex system from the engineering point of vie...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76681/1/AIAA-1988-4066-823.pd
This paper will talk about AIM 120 AMRAAM missile guidance for pursuing a moving target. The missile...
A new suboptimal guidance law is presented. It uses proportional navigation with phase lead compensa...
The efficacy of a munition depends on target detection, estimation of its motion, guidance, tracking...
The purpose of guidance is to cause a collision between a missile and a specified target. Accordingl...
In this study, it is aimed at comparing the performance of the guidance methods called Linear Homing...
Abstract — A missile system employed with homing guidance can sense and detect the target, guide its...