Sliding mode control based guidance law with impact time constraints


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

2013

Resumo

In this paper, the sliding mode control based guidance laws to intercept stationary targets at a desired impact time are proposed. Then, it is extended to constant velocity targets using the notion of predicted interception. The desired impact time is achieved by selecting the interceptor's lateral acceleration to enforce a sliding mode on a switching surface designed using non-linear engagement dynamics. Numerical simulation results are presented to validate the proposed guidance law for different initial engagement geometries, impact times and salvo attack scenarios

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/48082/1/Amer_Cont_Conf_5760_2013.pdf

Kumar, Shashi Ranjan and Ghose, Debasish (2013) Sliding mode control based guidance law with impact time constraints. In: 2013 American Control Conference (ACC), 17-19 June 2013, Washington, DC, pp. 5760-5765.

Publicador

IEEE

Relação

http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=6580740

http://eprints.iisc.ernet.in/48082/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Conference Paper

PeerReviewed