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Optimal principle for dynamical system with alterative orbiting

Репозитарій Національного Авіаційного Університету

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Field Value
 
Title Optimal principle for dynamical system with alterative orbiting
 
Creator Lysenko, O.I.
Tachinina, O.M.
 
Subject Optimization; Dynamic system; Branching path; Optimal trajectory
 
Description Lagrange problem with the account of functional limitation at any functional limitations at
any moment in a given interval is presented. The required conditions for optimal trajectories of the determinated dynamic system synthesized as space vehicle trajectories have been obtained.
 
Date 2017-06-15T19:30:20Z
2017-06-15T19:30:20Z
2016
 
Type Article
 
Identifier 1990-5548
http://er.nau.edu.ua/handle/NAU/29436
 
Language en_US
 
Format application/pdf
 
Publisher Electronics and Control Systems 2016. N 4(50): 108-113
 

Технічна підтримка: НДІІТТ НАУ