Optimal control model as an approach to the synthesis of a supersonic transport control system

被引：0
|
作者：
Irgaleev I.K. [1 ]
Efremov A.V. [1 ]
Grishina A.Y. [1 ]
Efremov E.V. [1 ]
机构：
[1] Moscow Aviation Institute (National Research University), Moscow
来源：
Aerospace Systems | 2025年 / 8卷 / 01期
关键词：
Control systems; Flying qualities; Inverse dynamics; Modified optimal control model; Optimal control model;
D O I：
10.1007/s42401-024-00291-4
中图分类号：
学科分类号：
摘要：
The present article considers a modified optimal control model (MOCM) of the pilot. The main idea behind the proposed modification is moving the time delay element, initially located at the input of the model, to its output. Such relocation eliminates the need for introducing a “predictor” block to the model’s structure, which simplifies the algorithm for calculating the parameters of the optimal model. Besides a description of the modified algorithm, the paper assesses the agreement between the performance achieved using the algorithm and the results of experimental investigations. In addition, the results of modeling are compared to the results obtained using a structural model. The comparison is carried out for a model of a second-generation supersonic transport for this vehicle. The MOCM’s potential in evaluating alternative flight control system laws is discussed as well. © Shanghai Jiao Tong University 2024.
引用
收藏
页码：117 / 124
页数：7
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