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 :
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