Lateral control of aircraft, considering the cross-coupling effect of yaw and roll on each-other using Fuzzy logic

Vishnu G. Nair; V. I. George; K. R. Prahlad

Lateral control of aircraft, considering the cross-coupling effect of yaw and roll on each-other using Fuzzy logic

Vishnu G. Nair, V. I. George, K. R. Prahlad

Department of Instrumentation and Control Engineering, Manipal Institute of Technology, Manipal

Research output: Contribution to specialist publication › Article

2 Citations (Scopus)

Abstract

In this paper, we explore fuzzy logic based approach for lateral control of aircrafts. Here the effect of roll on yaw and that of yaw on roll is taken into account. So the system will have greater accuracy and efficiency than the application of two separate controllers. This design will significantly reduce instability and increases maneuverability, as compared to existing control systems.

Original language	English
Pages	105-117
Number of pages	13
Volume	142
No.	7
Specialist publication	Sensors and Transducers
Publication status	Published - 2012

All Science Journal Classification (ASJC) codes

Control and Systems Engineering
Electrical and Electronic Engineering

Cite this

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abstract = "In this paper, we explore fuzzy logic based approach for lateral control of aircrafts. Here the effect of roll on yaw and that of yaw on roll is taken into account. So the system will have greater accuracy and efficiency than the application of two separate controllers. This design will significantly reduce instability and increases maneuverability, as compared to existing control systems.",

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PY - 2012

Y1 - 2012

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AB - In this paper, we explore fuzzy logic based approach for lateral control of aircrafts. Here the effect of roll on yaw and that of yaw on roll is taken into account. So the system will have greater accuracy and efficiency than the application of two separate controllers. This design will significantly reduce instability and increases maneuverability, as compared to existing control systems.

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Lateral control of aircraft, considering the cross-coupling effect of yaw and roll on each-other using Fuzzy logic

Abstract

All Science Journal Classification (ASJC) codes

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