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contributor authorYao Zhao
contributor authorYongzhi Sheng
contributor authorXiangdong Liu
contributor authorZhen Li
date accessioned2017-05-08T22:32:43Z
date available2017-05-08T22:32:43Z
date copyrightJuly 2016
date issued2016
identifier other49095875.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/82358
description abstractIn this paper, a nonlinear guidance law is developed for the approach and landing (A&L) phase of a reusable launch vehicle (RLV). First, a novel time-varying sliding mode control (TVSMC) technique is introduced. The main feature of this technique is that it enables the system states to converge to zero at the
publisherAmerican Society of Civil Engineers
titleAnalytic Approach and Landing Guidance through a Novel Time-Varying Sliding Mode Control Method
typeJournal Paper
journal volume29
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000581
treeJournal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 004
contenttypeFulltext


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