Minimum Time Control of the Rocket Attitude Reorientation Associated with Orbit Dynamics
نویسندگان
چکیده
منابع مشابه
Minimum Time Control of the Rocket Attitude Reorientation Associated with Orbit Dynamics
In this paper, we investigate the minimal time problem for the guidance of a rocket, whose motion is described by its attitude kinematics and dynamics but also by its orbit dynamics. Our approach is based on a refined geometric study of the extremals coming from the application of the Pontryagin maximum principle. Our analysis reveals the existence of singular arcs of higher-order in the optima...
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ژورنال
عنوان ژورنال: SIAM Journal on Control and Optimization
سال: 2016
ISSN: 0363-0129,1095-7138
DOI: 10.1137/15m1028716