DocumentCode :
3693582
Title :
Optimal guidance of the Isotropic Rocket in a partially uncertain flow field
Author :
Jhanani Selvakumar;Efstathios Bakolas
Author_Institution :
Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, 78712-1221, USA
fYear :
2015
fDate :
7/1/2015 12:00:00 AM
Firstpage :
3328
Lastpage :
3333
Abstract :
In this paper, we address the problem of characterizing the optimal strategy for guiding the so-called Isotropic Rocket to a fixed target in the presence of a partially known flowfield. We reformulate the guidance problem into an equivalent two-player pursuit evasion game, where the evader has a modified vectogram. First, we characterize the optimal strategies for both players, assuming that the evader is capturable. Then, we derive the necessary condition for capture, and visualize the capturability envelope using numerical simulations in which we compute the level sets of the optimal value function (isochrones). In addition, we consider a more general case of the game, where the pursuer is affected by friction (or drag). In that case, we identify the capture zones from geometric properties of the isochrones.
Keywords :
"Games","Rockets","Standards","Visualization","Friction","Game theory","Uncertainty"
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 2015 European
Type :
conf
DOI :
10.1109/ECC.2015.7331048
Filename :
7331048
Link To Document :
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