Impact Time Guidance for Large Heading Errors Using Sliding Mode Control
Data(s) |
2016
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Resumo |
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. |
Formato |
application/pdf |
Identificador |
http://eprints.iisc.ernet.in/53331/1/IEEE_Tra_Aer_Ele_Sys_51-4_3123_2016.pdf Kumar, Shashi Ranjan and Ghose, Debasish (2016) Impact Time Guidance for Large Heading Errors Using Sliding Mode Control. In: IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 51 (4). pp. 3123-3138. |
Publicador |
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC |
Relação |
http://dx.doi.org/10.1109/TAES.2015.140137 http://eprints.iisc.ernet.in/53331/ |
Palavras-Chave | #Aerospace Engineering (Formerly, Aeronautical Engineering) |
Tipo |
Journal Article PeerReviewed |