DocumentCode
3612971
Title
Impact time guidance for large heading errors using sliding mode control
Author
Kumar, Shashi Ranjan ; Ghose, Debasish
Author_Institution
Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
Volume
51
Issue
4
fYear
2015
Firstpage
3123
Lastpage
3138
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.
Keywords
variable structure systems; collision course; estimated interception time; impact time guidance; large heading angle errors; negative initial closing speeds; sliding mode control; Aerodynamics; Simulation; Sliding mode control; Time factors;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.2015.140137
Filename
7376242
Link To Document