Method for constructing automatic control systems with restriction on aircraft critical parameters

被引：0

作者：

Petunin V.I. ^{[1
]}

Neugodnikova L.M. ^{[1
]}

机构：

[1] Ufa State Technical University, ul. K. Marksa 12, Ufa, Bashkortostan

来源：

Russian Aeronautics | 2015年 / 58卷 / 03期

基金：

俄罗斯基础研究基金会;

关键词：

aircraft; algebraic selector; automatic control system; parameter restriction;

D O I：

10.3103/S1068799815030058

中图分类号：

学科分类号：

摘要：

The problem on restriction of aircraft motion parameters is considered. The special features are noted of constructing the logical dynamic systems of automatic control with algebraic selectors for different control channels of aircraft angular motion. The problems of synthesizing such systems are considered. The simulation results are presented. © 2015, Allerton Press, Inc.

引用

页码：279 / 285

页数：6

共 5 条

[1]

Mikhalev I.A., Okoemov B.N., Chikulaev M.S., Sistemy avtomaticheskogo upravleniya samoletom (The Aircraft Automatic Control Systems), (1987)

[2]

Petunin V.I., Synthesis of Automatic Control System for Aircraft Based on Automatic Restriction of Limiting Parameters, Izv. Vuz. Priborostroenie, 53, 10, pp. 18-24, (2010)

[3]

Petunin V.I., Synthesis of Logic-Dynamic Automatic Control Systems of Gas Turbine Engines Based on Control Channels Matching and Adaptation, Doctorate (Tech.) Dissertation, (2011)

[4]

Petunin V.I., Neugodnikova L.M., Synthesis of Aircraft Automatic Control System of Course Angle and Normal Overload Restriction, Aviakosmicheskoe Priborostroenie, 1, pp. 10-18, (2012)

[5]

Petunin V.I., Synthesis of Control Laws of a Pitch Channel of the Autopilot, Vestnik UGATU, 9, 2, pp. 25-31, (2007)

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