Optimal principle for dynamical system with alterative orbiting
| dc.contributor.author | Lysenko, O.I. | en |
| dc.contributor.author | Tachinina, O.M. | en |
| dc.date.accessioned | 2017-06-15T19:30:20Z | |
| dc.date.available | 2017-06-15T19:30:20Z | |
| dc.date.issued | 2016 | |
| dc.description.abstract | 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. | en |
| dc.identifier.issn | 1990-5548 | |
| dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/29436 | |
| dc.language.iso | en | en |
| dc.publisher | Electronics and Control Systems 2016. N 4(50).- p.108-113 | en |
| dc.subject | optimization | en |
| dc.title | Optimal principle for dynamical system with alterative orbiting | en |
| dc.type | Article | en |