We at Lawrence Livermore National Laboratory (LLNL) have developed a new missile guidance law for intercepting a missile during boost phase. Unlike other known missile guidance laws being used today, the new t-Dv guidance law optimally trades an interceptor’s onboard fuel capacity against time-to-go before impact. In particular, this guidance law allows a missile designer to program the interceptor to maximally impact a boosting missile before burnout or burn termination and thus negating its ability to achieve the maximum kinetic velocity. For an intercontinental range ballistic missile (ICBM), it can be shown that for every second of earlier intercept prior to burnout, the ICBM ground range is reduce
We present a novel guidance law that uses observations consisting solely of seeker line-of-sight ang...
[[abstract]]How to develop a novel missile guidance law that can act effectively against very high s...
A Mid-course guidance algorithm has been developed for an exo-atmospheric interceptor to neutralize ...
Lawrence Livermore National Laboratory (LLNL) have developed a new missile guidance law for intercep...
The paper presents a near-optimal guidance law that has been developed using the direct method of ca...
International audiencePurpose – This note aims to introduce a terminal guidance law that is able to ...
This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of...
This paper focuses on missile guidance methods for a “defense” missile trying to protect a cooperati...
Intercontinental Ballistic Missiles are capable of placing a nuclear warhead at more than 5,000 km a...
Current Ballistic Missile (BM) defence systems intercept an incoming threat in its terminal phase, a...
ABSTRACT: This paper presents a comprehensive study on the performance analysis of 8 conceptual guid...
A new, highly constrained guidance law is proposed against a maneuvering target while satisfying bot...
We present a novel guidance law that uses observations consisting solely of seeker line of sight ang...
An optimal impact angle control guidance law is proposed in this paper.The missile system is approxi...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
We present a novel guidance law that uses observations consisting solely of seeker line-of-sight ang...
[[abstract]]How to develop a novel missile guidance law that can act effectively against very high s...
A Mid-course guidance algorithm has been developed for an exo-atmospheric interceptor to neutralize ...
Lawrence Livermore National Laboratory (LLNL) have developed a new missile guidance law for intercep...
The paper presents a near-optimal guidance law that has been developed using the direct method of ca...
International audiencePurpose – This note aims to introduce a terminal guidance law that is able to ...
This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of...
This paper focuses on missile guidance methods for a “defense” missile trying to protect a cooperati...
Intercontinental Ballistic Missiles are capable of placing a nuclear warhead at more than 5,000 km a...
Current Ballistic Missile (BM) defence systems intercept an incoming threat in its terminal phase, a...
ABSTRACT: This paper presents a comprehensive study on the performance analysis of 8 conceptual guid...
A new, highly constrained guidance law is proposed against a maneuvering target while satisfying bot...
We present a novel guidance law that uses observations consisting solely of seeker line of sight ang...
An optimal impact angle control guidance law is proposed in this paper.The missile system is approxi...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
We present a novel guidance law that uses observations consisting solely of seeker line-of-sight ang...
[[abstract]]How to develop a novel missile guidance law that can act effectively against very high s...
A Mid-course guidance algorithm has been developed for an exo-atmospheric interceptor to neutralize ...