ELECTRICA

MULTIVARIABLE CONTROL IN HELICOPTERS

1.

University of Hartford, West Hartford, CT, USA

2.

İstanbul University, Department of Electrical & Electronics Engineering, 34320, Avcılar, İstanbul, Turkey

ELECTRICA 2002; 2: 437-446
Read: 693 Downloads: 422 Published: 28 December 2019

In this paper, general control approaches are evaluated for helicopter system. Control of a helicopter is its ability to respond to control inputs and achieve the desired condition of flight. There is an important contradiction between stability and controllability, since decent controllability does not necessarily exist with decent stability. In fact, a high degree of stability may tend to reduce the controllability of the aircraft.

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EISSN 2619-9831