Direct Method for Forming the Optimal Open Loop Control of Aerial Vehicles
- 作者: Korsun O.1,2, Stulovskii A.1,3
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隶属关系:
- State Research Institute of Aviation Systems
- Moscow Institute of Aviation (National Research University)
- Moscow Institute of Physics and Technology
- 期: 卷 58, 编号 2 (2019)
- 页面: 229-243
- 栏目: Control Systems for Technological Processes
- URL: https://journals.rcsi.science/1064-2307/article/view/220329
- DOI: https://doi.org/10.1134/S1064230719020114
- ID: 220329
如何引用文章
详细
A direct method for finding the optimal open loop control of an aircraft is proposed. It is based on the preliminary parameterization of controls with the subsequent parameter estimation using the numerical minimization of a given functional. Conditions for the application of this method and possible constraints are discussed. The efficiency of the method is confirmed by examples that use the results of simulation and flight data. The results are compared with the solutions obtained using the classical approach to finding the optimal control based on the solution of a two-point boundary value problem.
作者简介
O. Korsun
State Research Institute of Aviation Systems; Moscow Institute of Aviation (National Research University)
编辑信件的主要联系方式.
Email: marmotto@rambler.ru
俄罗斯联邦, Moscow, 125319; Moscow, 125993
A. Stulovskii
State Research Institute of Aviation Systems; Moscow Institute of Physics and Technology
Email: marmotto@rambler.ru
俄罗斯联邦, Moscow, 125319; Dolgoprudnyi, Moscow oblast, 141700
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