Add to ORKGAccurate calculation of time to go until impact is an essential component in coordinating multiple precision-guided munitions for a simultaneous strike. Conventional means for calculating time to go contain potential errors, due in part to the trajectory curvatures, and may fall short on the accuracy required to achieve a desired impact time, especially if velocity changes rapidly due to atmospheric drag and gravity. A closed-loop guidance law will be presented in which an optimized, piecewise continuous, and smooth family of polynomial trajectories is parameterized in terms of downrange distance and has a closed-form solution of arc length for improved calculation of time to go
To address the need for flexible energy management and impact angle control in the midcourse guidanc...
The authors propose an autopilot based on partial integrated guidance and control for missiles to ac...
In the guidance literature, minimizing miss distance along with optimizing the energy usage had been...
Standard optimal guidance laws are formulated using linear dynamic constraints and are typically exp...
A new missile guidance law is proposed for the control of impact time which provides an improved tim...
This paper discusses the problem of impact time control of an interceptor against a stationary targe...
A finite-time-convergent impact time control guidance law based on pure proportional navigation is p...
The problem of controlling the engagement time of an interceptor against a stationary target is cons...
This study presents a novel impact time and angle constrained guidance law for homing missiles. The ...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
AbstractThis study presents a novel impact time and angle constrained guidance law for homing missil...
This paper proposes a novel approach for guidance law design to satisfy the impact-time constraints ...
This paper presents an impact-angle-control guidance law with terminal constraints on the curvature ...
This paper proposes a guidance strategy, which caters to both impact angle and impact time terminal ...
Autonomous aerial vehicles like missiles and unmanned aerial vehicles (UAVs) have attracted various ...
To address the need for flexible energy management and impact angle control in the midcourse guidanc...
The authors propose an autopilot based on partial integrated guidance and control for missiles to ac...
In the guidance literature, minimizing miss distance along with optimizing the energy usage had been...
Standard optimal guidance laws are formulated using linear dynamic constraints and are typically exp...
A new missile guidance law is proposed for the control of impact time which provides an improved tim...
This paper discusses the problem of impact time control of an interceptor against a stationary targe...
A finite-time-convergent impact time control guidance law based on pure proportional navigation is p...
The problem of controlling the engagement time of an interceptor against a stationary target is cons...
This study presents a novel impact time and angle constrained guidance law for homing missiles. The ...
A guidance problem for impact time and angle control applicable to cooperative attack is considered ...
AbstractThis study presents a novel impact time and angle constrained guidance law for homing missil...
This paper proposes a novel approach for guidance law design to satisfy the impact-time constraints ...
This paper presents an impact-angle-control guidance law with terminal constraints on the curvature ...
This paper proposes a guidance strategy, which caters to both impact angle and impact time terminal ...
Autonomous aerial vehicles like missiles and unmanned aerial vehicles (UAVs) have attracted various ...
To address the need for flexible energy management and impact angle control in the midcourse guidanc...
The authors propose an autopilot based on partial integrated guidance and control for missiles to ac...
In the guidance literature, minimizing miss distance along with optimizing the energy usage had been...