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Impact time guidance for large heading errors using sliding mode control.

Authors :
Kumar, Shashi Ranjan
Ghose, Debasish
Source :
IEEE Transactions on Aerospace & Electronic Systems. Oct2015, Vol. 51 Issue 4, p3123-3138. 16p.
Publication Year :
2015

Abstract

In this paper, sliding mode control-based impact time guidance laws are proposed. Even for large heading angle errors and negative initial closing speeds, the desired impact time is achieved by enforcing a sliding mode on a switching surface designed by using the concepts of collision course and estimated time-to-go. Unlike existing guidance laws, the proposed guidance strategy achieves impact time successfully even when the estimated interception time is greater than the desired impact time. Simulation results are also presented. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
00189251
Volume :
51
Issue :
4
Database :
Academic Search Index
Journal :
IEEE Transactions on Aerospace & Electronic Systems
Publication Type :
Academic Journal
Accession number :
112245987
Full Text :
https://doi.org/10.1109/TAES.2015.140137