DocumentCode
1301970
Title
Performance Analysis of Guidance Laws Based on Timescale Gap
Author
Dhananjay, Narayanachar ; Ghose, Debasish ; Bhat, M. Seetharama
Author_Institution
Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
Volume
18
Issue
3
fYear
2010
fDate
5/1/2010 12:00:00 AM
Firstpage
574
Lastpage
590
Abstract
An analytical treatment of performance analysis of guidance laws is possible only in simplistic scenarios. As the complexity of the guidance system increases, a search for analytical solutions becomes quite impractical. In this paper, a new performance measure, based upon the notion of a timescale gap that can be computed through numerical simulations, is developed for performance analysis of guidance laws. Finite time Lyapunov exponents are used to define the timescale gap. It is shown that the timescale gap can be used for quantification of the rate of convergence of trajectories to the collision course. Comparison between several guidance laws, based on the timescale gap, is presented. Realistic simulations to study the effect of aerodynamics and atmospheric variations on the timescale gap of these guidance laws are also presented.
Keywords
Lyapunov methods; collision avoidance; differential geometry; game theory; missile guidance; nonlinear control systems; numerical analysis; collision course; finite time Lyapunov exponents; guidance laws analysis; numerical simulations; performance analysis; timescale gap; trajectory convergence rate; Guidance laws; nonlinear systems; proportional navigation; timescale gap;
fLanguage
English
Journal_Title
Control Systems Technology, IEEE Transactions on
Publisher
ieee
ISSN
1063-6536
Type
jour
DOI
10.1109/TCST.2009.2024534
Filename
5208380
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