Control and trajectory optimization of an aircraft’s alignment with the desired track
- 作者: Volodina Y.1, Golubeva A.1, Kulanov N.1
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隶属关系:
- State Research Institute of Aviation Systems
- 期: 卷 56, 编号 5 (2017)
- 页面: 837-861
- 栏目: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219982
- DOI: https://doi.org/10.1134/S1064230717040165
- ID: 219982
如何引用文章
详细
The synthesis of the control with the optimal trajectory length is constructed for the problem of aligning an aircraft with the desired track with the ground speed vector direction along the desired track. The solution is based on the maximum principle and involves the use of numerical methods for solving the boundary value problem and analytical investigations for determining the set of possible extremals and comparing the lengths of the trajectories when selecting the optimal one. As a result of these investigations, the switching and separation lines are determined that bound the regions in the phase space which correspond to different values of the optimal relay control.
作者简介
Yu. Volodina
State Research Institute of Aviation Systems
Email: aagolubeva@2100.gosniias.ru
俄罗斯联邦, Moscow
A. Golubeva
State Research Institute of Aviation Systems
编辑信件的主要联系方式.
Email: aagolubeva@2100.gosniias.ru
俄罗斯联邦, Moscow
N. Kulanov
State Research Institute of Aviation Systems
Email: aagolubeva@2100.gosniias.ru
俄罗斯联邦, Moscow
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