DocumentCode
3686226
Title
Selection of optimal time-to-go in generalized vector explicit guidance
Author
Sabyasachi Mondal;Radhakant Padhi
Author_Institution
Department of Aerospace Engineering, Indian Institute of Science, Bangalore, Karnataka, 560012
fYear
2015
Firstpage
756
Lastpage
761
Abstract
A new method of selection of time-to-go (tgo) for Generalized Vector Explicit Guidance (GENEX) law have been proposed in this paper. tgo is known to be an important parameter in the control and cost function of GENEX guidance law. In this paper the formulation has been done to find an optimal value of tgo that minimizes the performance cost. Mechanization of GENEX with this optimal tgo reduces the lateral acceleration demand and consequently increases the range of the interceptor. This new formulation of computing tgo comes in closed form and thus it can be implemented onboard. This new formulation is applied in the terminal phase of an surface-to-air interceptor for an angle constrained engagement. Results generated by simulation justify the use of optimal tgo.
Keywords
"Missiles","Acceleration","Cost function","Optimal control","Radio frequency","Geometry","Closed-form solutions"
Publisher
ieee
Conference_Titel
Control Applications (CCA), 2015 IEEE Conference on
Type
conf
DOI
10.1109/CCA.2015.7320708
Filename
7320708
Link To Document