Name
Title | ||
|---|---|---|
Three dimensional retro-PN based impact time control for higher speed nonmaneuvering targets |
Abstract | ||
|---|---|---|
In the implementation of modern guidance laws, especially in impact time constrained engagement scenario or multiple agent salvo attack scenario, a good estimate of time-to-go is extremely crucial. The most widely used time-to-go estimate range over closing speed has several limitations. Very few work is there in existing literature which actually try to estimate the time-to-go. Most of them are meant for the engagement of lower speed target with a higher speed interceptor. However, in the current defence scenario, targets of higher speed than the interceptor is a reality. This paper first discusses a recursive time-to-go estimation method for three dimensional engagement of a Retro-PN guided interceptor with higher speed non-maneuvering target and then presents a navigation gain scheduling algorithm to achieve the interception at a pre-specified time. The effectiveness of the time-to-go estimation method and the gain scheduling algorithm is justified with simulation results. |
Year | DOI | Venue |
|---|---|---|
2013 | 10.1109/CDC.2013.6760652 | Decision and Control |
Keywords | Field | DocType |
estimation theory,missile guidance,optimal control,higher speed nonmaneuvering targets,missile guidance laws,multiple agent salvo attack scenario,navigation gain scheduling algorithm,retro-PN guided interceptor,three dimensional retro-PN based impact time control,time-to-go estimation method | Optimal control,Computer science,Gain scheduling,Control theory,Simulation,Supercomputer Education Research Centre,Estimation theory,Missile guidance,Recursion | Conference |
ISSN | ISBN | Citations |
0743-1546 | 978-1-4673-5714-2 | 1 |
PageRank | References | Authors |
0.39 | 3 | 3 |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Satadal Ghosh | 1 | 5 | 2.15 |
| Debasish Ghose | 2 | 777 | 71.57 |
| Soumyendu Raha | 3 | 44 | 9.60 |