Longitudinal Absolute Stability of a BWB Aircraft-Pilot System with Saturated Actuator Model

Longitudinal Absolute Stability of a BWB Aircraft-Pilot System with Saturated Actuator Model

This paper deals with the analysis of the P(ilot) I(n-the-Loop) O(scillations) of the second category (with rate and position liming in the closed loop pilot-vehicle system), caused by the dynamic coupling between the human pilot and the aircraft. The analysis is made in the context of the longitudi...

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Bibliographic Details
Main Author: Claudia Alice STATE
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2013-09-01
Series:INCAS Bulletin
Subjects:
scillations
Popov criterion
frequency domain inequality
Blended Wing Body
actuator saturatio
Online Access:http://bulletin.incas.ro/files/state_c_a__v5_iss_3_full.pdf

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