The main contribution of this study is the optimality analysis of the PPNG performed in full generality. The new theoretical findings can explain the result of the former analysis in which the PPNG is derived as the minimum effort solution [5] and also describe a comprehensive design framework including the observability-enhanced guidance laws developed for the dual homing guidance problem. Furthermore, this study provides several examples illustrating how the PPNG with various navigation gain functions can be understood as optimal control solutions
International audiencePurpose – This note aims to introduce a terminal guidance law that is able to ...
A new form of the Proportional Navigation (PN) guidance law for short-range homing missiles is propo...
A new form of the Proportional Navigation (PN) guidance law for short-range homing missiles is propo...
This dissertation studies the optimal guidance of homing missiles. The guidance objective is to dete...
This study outlines the set of equations constituting the necessary conditions that should be solved...
This paper proposes a new optimal guidance law based on proportional-integral (PI) concept to reduce...
Abstract — A missile system employed with homing guidance can sense and detect the target, guide its...
An analytical treatment of the biased proportional navigation (BPN) is carried out with the aim of o...
Starting from a definition of the biased proportional navigation (PN) law and expression of the traj...
Guidance is defined as the determination of a strategy for following a nominal path in the presence ...
A new suboptimal guidance law is presented. It uses proportional navigation with phase lead compensa...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76681/1/AIAA-1988-4066-823.pd
An optimal impact angle control guidance law is proposed in this paper.The missile system is approxi...
This study presents a novel extension to the theory of optimal guidance laws represented by the nont...
This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of...
International audiencePurpose – This note aims to introduce a terminal guidance law that is able to ...
A new form of the Proportional Navigation (PN) guidance law for short-range homing missiles is propo...
A new form of the Proportional Navigation (PN) guidance law for short-range homing missiles is propo...
This dissertation studies the optimal guidance of homing missiles. The guidance objective is to dete...
This study outlines the set of equations constituting the necessary conditions that should be solved...
This paper proposes a new optimal guidance law based on proportional-integral (PI) concept to reduce...
Abstract — A missile system employed with homing guidance can sense and detect the target, guide its...
An analytical treatment of the biased proportional navigation (BPN) is carried out with the aim of o...
Starting from a definition of the biased proportional navigation (PN) law and expression of the traj...
Guidance is defined as the determination of a strategy for following a nominal path in the presence ...
A new suboptimal guidance law is presented. It uses proportional navigation with phase lead compensa...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76681/1/AIAA-1988-4066-823.pd
An optimal impact angle control guidance law is proposed in this paper.The missile system is approxi...
This study presents a novel extension to the theory of optimal guidance laws represented by the nont...
This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of...
International audiencePurpose – This note aims to introduce a terminal guidance law that is able to ...
A new form of the Proportional Navigation (PN) guidance law for short-range homing missiles is propo...
A new form of the Proportional Navigation (PN) guidance law for short-range homing missiles is propo...