Impact Time Guidance for Large Heading Errors Using Sliding Mode Control


Autoria(s): Kumar, Shashi Ranjan; Ghose, Debasish
Data(s)

2016

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