Injection into Orbit Optimization using Orthogonal Polynomials

In this study, the problem of determining an optimal trajectory of a nonlinear injection into orbit problem with minimum time was investigated. The method was based on orthogonalpolynomial approximation. This method consisted of reducing the optimal control problem to a system of algebraic equations...

Full description

Bibliographic Details
Main Authors: Sedigheh Shahmirzaee Jeshvaghany, Farshad Pazooki, Alireza Basohbat Novinzaddeh
Format: Article
Language:English
Published: Islamic Azad University-Isfahan (Khorasgan) Branch 2017-01-01
Series:International Journal of Advanced Design and Manufacturing Technology
Subjects:
Online Access:https://admt.isfahan.iau.ir/article_534981_391af4ea3ebdae5c70bf2aaf3220fe75.pdf