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contributor authorGang Zhang
contributor authorHuidong Ma
contributor authorMing Liu
date accessioned2022-08-18T12:18:13Z
date available2022-08-18T12:18:13Z
date issued2022/06/09
identifier other%28ASCE%29AS.1943-5525.0001464.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4286387
description abstractThis paper proposes a new method to solve Lambert’s problem with multiple constraints, including the impulse-magnitude constraints, the trajectory-radius constraints, and the terminal-impact-angle constraint. First, the closed-form range of the chordal terminal velocity component for each constraint is derived. Then, the admissible intersection range for all constraints is obtained. Finally, the feasible solutions are solved in the admissible intersection range by using the terminal-velocity-based Lambert algorithm. The 180° case and the multiple-revolution case are also considered. The proposed method can be also extended to the Lambert algorithms with other independent variables. Compared with the typical method of first solving Lambert’s problem and then pruning the solutions that do not satisfy the constraints, the numerical examples show that the proposed method can reduce a lot of computational time.
publisherASCE
titleLambert’s Problem with Multiple Constraints
typeJournal Article
journal volume35
journal issue5
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0001464
journal fristpage04022066
journal lastpage04022066-9
page9
treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 005
contenttypeFulltext


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