Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77380/1/AIAA-1998-4547-770.pd
International audiencePurpose – This note aims to introduce a terminal guidance law that is able to ...
In the last decades a number of countries have shown interest towards anti-satellite systems for str...
A new, highly constrained guidance law is proposed against a maneuvering target while satisfying bot...
In a Newtonian central force field, the minimum-fuel interception of a satellite, or a ballistic mis...
Interception of target rocket moving along a trajectory in a gravitational field by an interceptor r...
For several decades, guidance problems for interception have been extensively studied, and some guid...
ABSTRACT: This paper presents a comprehensive study on the performance analysis of 8 conceptual guid...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
AbstractThis article aims to develop a head pursuit (HP) guidance law for three-dimensional hypervel...
Intercontinental Ballistic Missiles are capable of placing a nuclear warhead at more than 5,000 km a...
This paper proposes a synthesis of new guidance law to generate an evasive maneuver against enemy’s ...
Optimal control theory is applied to the study of missile evasion, particularly in the case of a sin...
A method for determining the optimal impulsive trajectories is applied to minimum fuel, direct ascen...
This paper studies the proximate satellite interception guidance strategies where both the intercept...
In this paper, some new results on time-varying missile against a stationary target using pure propo...
International audiencePurpose – This note aims to introduce a terminal guidance law that is able to ...
In the last decades a number of countries have shown interest towards anti-satellite systems for str...
A new, highly constrained guidance law is proposed against a maneuvering target while satisfying bot...
In a Newtonian central force field, the minimum-fuel interception of a satellite, or a ballistic mis...
Interception of target rocket moving along a trajectory in a gravitational field by an interceptor r...
For several decades, guidance problems for interception have been extensively studied, and some guid...
ABSTRACT: This paper presents a comprehensive study on the performance analysis of 8 conceptual guid...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
AbstractThis article aims to develop a head pursuit (HP) guidance law for three-dimensional hypervel...
Intercontinental Ballistic Missiles are capable of placing a nuclear warhead at more than 5,000 km a...
This paper proposes a synthesis of new guidance law to generate an evasive maneuver against enemy’s ...
Optimal control theory is applied to the study of missile evasion, particularly in the case of a sin...
A method for determining the optimal impulsive trajectories is applied to minimum fuel, direct ascen...
This paper studies the proximate satellite interception guidance strategies where both the intercept...
In this paper, some new results on time-varying missile against a stationary target using pure propo...
International audiencePurpose – This note aims to introduce a terminal guidance law that is able to ...
In the last decades a number of countries have shown interest towards anti-satellite systems for str...
A new, highly constrained guidance law is proposed against a maneuvering target while satisfying bot...
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