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contributor authorJian Yang
contributor authorZhihua Qu
contributor authorJing Wang
contributor authorRichard A. Hull
date accessioned2017-05-08T21:16:29Z
date available2017-05-08T21:16:29Z
date copyrightOctober 2009
date issued2009
identifier other%28asce%290893-1321%282009%2922%3A4%28331%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45178
description abstractThe problem of determining an optimal feasible trajectory, for a fixed wing flying vehicle moving in a dynamical three-dimensional space, is addressed in this paper, and an analytical solution is proposed. With explicitly considering the boundary conditions and kinematic constraints as well as by satisfying the collision avoidance criterions, trajectories are described in terms of three parameterized polynomials, and the family of feasible trajectories are found. Then, the desired near shortest trajectory is chosen from the feasible trajectories by optimizing a performance index with respect to
publisherAmerican Society of Civil Engineers
titleReal-Time Optimized Trajectory Planning for a Fixed-Wing Vehicle Flying in a Dynamic Environment
typeJournal Paper
journal volume22
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2009)22:4(331)
treeJournal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 004
contenttypeFulltext


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