Lunar Ascent and Orbit Injection via Neighboring Optimal Guidance and Constrained Attitude Control
نویسندگان
چکیده
منابع مشابه
On the optimal guidance for planar Lunar ascent
The paper is focused on the equations of the optimal guidance for planar Lunar ascent. We point out some computational and graphical aspects.
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ژورنال
عنوان ژورنال: Journal of Aerospace Engineering
سال: 2018
ISSN: 0893-1321,1943-5525
DOI: 10.1061/(asce)as.1943-5525.0000908