The thrust minimization problem and its applications

Ivanyukhin, A. V.; Petukhov, V. G.

doi:10.1134/s0010952515040048

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Cited by 11 publications

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“…where γ is the magnitude of the spacecraft acceleration, typically due to the propulsion system, while t 0 and t f are the initial and final time of spaceflight. This representation is popular in researches including thrust minimization [100], [71]. Other forms of cost functions for acceleration are popular in spacecraft trajectory optimization problems, specifically in shape-based techniques [101].…”

Section: Accelerationmentioning

confidence: 99%

Spacecraft trajectory optimization: A review of models, objectives, approaches and solutions

Shirazi

Ceberio

Lozano

2018

Progress in Aerospace Sciences

118

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This article is a survey paper on solving spacecraft trajectory optimization problems. The solving process is decomposed into four key steps of mathematical modeling of the problem, defining the objective functions, development of an approach and obtaining the solution of the problem. Several subcategories for each step have been identified and described. Subsequently, important classifications and their characteristics have been discussed for solving the problems. Finally, a discussion on how to choose an element of each step for a given problem is provided.

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Section: Accelerationmentioning

confidence: 99%