Study of Design and Optimization of Low-Thrust Transfer Trajectory with Planetary Aerogravity Assist

Shang, Haibin; Cui, Pingyuan; Luan, Enjie; Dong, Qiao

doi:10.1109/cesa.2006.4281741

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Modified Equinoctial Orbital Elements1

Initial and Terminal Conditions1

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2018

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(2 citation statements)

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“…Also, f N , f S , and f W are components of the perturbing acceleration in the directions perpendicular to the radius vector in the direction of motion, along the outward radius vector, and normal to the orbital plane in the direction of the angular momentum vector, respectively. This set of equations is employed in a lot of research with various space missions including interplanetary transfers with gravity assist maneuvers [50], [51]. Besides, the use of modified equinoctial elements to describe the osculating orbits is a good choice due to the easy formulation and robustness to uncertainties.…”

Section: Modified Equinoctial Orbital Elementsmentioning

confidence: 99%

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

Shirazi

Ceberio

Lozano

2018

Progress in Aerospace Sciences

119

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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: Modified Equinoctial Orbital Elementsmentioning

confidence: 99%

“…31. This kind of cost function is used in several articles including gravity assist maneuvers [50], [51], continuous interplanetary trajectories [96], spacecraft reentry [98] and orbit rising mission [99].…”

Section: Initial and Terminal Conditionsmentioning

confidence: 99%