NDLI: Robust, decoupled, flight control design with rate saturating actuators

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Robust, decoupled, flight control design with rate saturating actuators

Content Provider	NASA Technical Reports Server (NTRS)
Author	Hess, R. A. Snell, S. A.
Copyright Year	1997
Description	Techniques for the design of control systems for manually controlled, high-performance aircraft must provide the following: (1) multi-input, multi-output (MIMO) solutions, (2) acceptable handling qualities including no tendencies for pilot-induced oscillations, (3) a tractable approach for compensator design, (4) performance and stability robustness in the presence of significant plant uncertainty, and (5) performance and stability robustness in the presence actuator saturation (particularly rate saturation). A design technique built upon Quantitative Feedback Theory is offered as a candidate methodology which can provide flight control systems meeting these requirements, and do so over a considerable part of the flight envelope. An example utilizing a simplified model of a supermaneuverable fighter aircraft demonstrates the proposed design methodology.
File Size	831753
Page Count	13
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19980021298
Archival Resource Key	ark:/13960/t1hj1fz9w
Language	English
Publisher Date	1997-01-01
Access Restriction	Open
Subject Keyword	Aircraft Stability And Control Actuators Robustness Mathematics Stability Control Systems Design Manual Control Mimo Control Systems Controllability Pilot Induced Oscillation Flight Control Fighter Aircraft Flight Envelopes Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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