Материалов:
1 005 012

Репозиториев:
30

Авторов:
596 024

По вашему запросу найдено документов: 17502

Страница 1 из 1751

Optimization of Multi-revolution Limited Power Trajectories Using Angular Independent Variable
Ivanyukhin A., Petukhov V.
Optimization of low-thrust trajectories is necessary in the design of space missions using electric
Low-Thrust Lunar Trajectory Optimization Using Canonical Transformation
Yoon S.W., Petukhov V.G., Ivanyukhin A.V.
studies. This technique allows us to obtain the results of near-optimal trajectory with insignificant
Stabilization of Optimal Trajectories of Dynamical Systems
Kaspirovich I.E., Mukharlyamov R.G.
as an inverse problem of dynamics. The requirement to limit deviations from the optimal trajectory is considered
Optimization of the finite-thrust trajectory in the vicinity of a circular orbit
Petukhov V.G., Olívio A.P.
The paper considers the problem of the optimization of the finite-thrust trajectory in the vicinity
Control System Synthesis Based on Optimal Trajectories Approximation by Symbolic Regression for Group of Robots
Konstantinov S.V., Diveev A.I.
to solve this problem based on the approximation of the set of optimal trajectories using symbolic
An approach for end-to-end optimization of low-thrust interplanetary trajectories using collinear libration points
Yoon S.W., Petukhov V., Ivanyukhin A.
-thrust interplanetary trajectory. At first, the problem of optimizing low-thrust interplanetary trajectory, which passes
Evaluation of optimal low-thrust interplanetary trajectories with collinear libration points transitions
Yoon S.W., Petukhov V.G., Ivanyukhin A.V.
of the interplanetary low-thrust trajectory. At first, the problem of optimizing low-thrust interplanetary trajectory
Synthesis of Trajectory Planning Algorithms Using Evolutionary Optimization Algorithms
Malyshev D., Cherkasov V., Rybak L., Diveev A.
The article considers the problem of planning the optimal trajectory of a delta robot
Optimization of finite-thrust trajectories with fixed angular distance
Petukhov V., Ivanyukhin A., Popov G., Testoyedov N., Yoon S.W.
The article presents a new approach for optimizing the trajectories of spacecraft with finite
Minimum-Thrust Lunar Trajectories
Yoon S.W., Petukhov V.G., Ivanyukhin A.V.
and of the continuation method is used. The optimization problem for the considered type of trajectories gave rise

Страница 1 из 1751

Фасеты

Новости проекта

Новости

Партнеры

КФУ
ТГУ
Elpub
СФУ
Webpublishers

Индексация

BASE
WorldCat
OpenAIRE
EDS
core