Aircraft longitudinal control without a pitch command in the autopilot

被引：0
作者：
Romanenko L.G. [1 ]
Romanenko A.G. [1 ]
Samarova G.G. [2 ]
机构：
[1] Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, Kazan, Tatarstan
[2] OAO OKB Sokol, ul. Akademika Parina 2a, Kazan, Tatarstan
来源：
Russian Aeronautics | 2014年 / 57卷 / 04期
关键词：
aircraft longitudinal motion; autopilot; optimal gain selection in elevator channel;
D O I：
10.3103/S1068799814040072
中图分类号：
学科分类号：
摘要：
The laws of longitudinal motion control without data on the pitch angle are proposed. A procedure for analytical selection of the optimal gain in the elevator channel is proposed. The results of simulating the aircraft-autopilot system are presented. © 2014, Allerton Press, Inc.
引用
收藏
页码：361 / 367
页数：6
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