Absolute stability for the lateral-directional BWB model with rate limited actuator

Journal Title: INCAS BULLETIN - Year 2012, Vol 4, Issue 2

Abstract

In this paper the authors present a study regarding the interaction between the human pilot and the aircraft which may result in a dangerous phenomenon called Pilot Induced Oscillations (PIO), in the context of the lateral directional motion. The theoretical model of the airplane used is a Blended Wing Body (BWB) configuration and the human operator is expressed by the Synchronous Pilot Model (represented by a simple gain). The Popov criterion, in the case of the infinite parameter, is applied in order to investigate the absolute stability of the pilot-airplane linearized system in the presence of the rate saturation of the actuator.

Authors and Affiliations

Ionel IORGA, Claudia STATE

Keywords

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  • EP ID EP140396
  • DOI 10.13111/2066-8201.2012.4.2.12
  • Views 78
  • Downloads 0

How To Cite

Ionel IORGA, Claudia STATE (2012). Absolute stability for the lateral-directional BWB model with rate limited actuator. INCAS BULLETIN, 4(2), 115-123. https://europub.co.uk./articles/-A-140396