Pareto-optimal parametric programs for spacecraft relative motion control at near circular orbits

Мұқаба

Дәйексөз келтіру

Толық мәтін

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Рұқсат жабық Рұқсат берілді
Рұқсат жабық Тек жазылушылар үшін

Аннотация

The problem of designing a set of nominal Pareto optimal control programs for the relative motion of a spacecraft maneuvering in circular orbits relative to a passive target is considered. Motion is considered in an orbital cylindrical reference frame in variables characterizing secular and periodic motion in a dimensionless form, invariant with respect to the magnitude of acceleration from the thrust of a maneuvering spacecraft and the height of the reference orbit. On the basis of analytical studies, areas of boundary conditions have been constructed that allow the use of simpler relative motion control programs with two active areas oriented in the transversal direction. The solution of a two-criterion parametric problem for the criteria is obtained: the motor operating time of the engine, and the total duration of the maneuver. The application of the Pareto optimality principle made it possible to simplify the numerical procedure for constructing the desired set of non-improved solutions to the problem from the available sample satisfying the boundary conditions of the transfer.

Толық мәтін

Рұқсат жабық

Авторлар туралы

S. Ishkov

Samara University

Email: filippov.ga@ssau.ru
Ресей, Samara

G. Filippov

Samara University

Хат алмасуға жауапты Автор.
Email: filippov.ga@ssau.ru
Ресей, Samara

Әдебиет тізімі

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2. Fig. 1. Analysis of secular motion trajectories

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3. Fig. 2. Pareto set of optimal solutions to the problem for the boundary conditions small deviation and large deviation

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4. Fig. 3. An example of a secular motion trajectory (top) and the dependence of the minor semi-axis of the relative motion ellipse on time (bottom), program control with two thrust activations of different signs

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5. Fig. 4. An example of a secular motion trajectory (top) and the dependence of the minor semi-axis of the relative motion ellipse on time (bottom), program control with two thrust activations of the same sign

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