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Activity title

AG-300 V.33 Flight Test Techniques for the Assessment of Fixed-Wing Aircraft Handling Qualities

Activity Reference

SCI-303

Panel

Systems Concepts and Integration

Security Classification

PUBLIC RELEASE

Status

Active

Activity type

AG

Start date

2018

End date

2021

Keywords

Aircraft Pilot Coupling APC, Boundary Avoidance Tracking BAT, Data processing, Flight Testing, Ground Attack Test Equipment GRATE, Handling Qualities, Handling Qualities During Tracking HQDT, Instrumentation, Pilot Involved Oscillations PIO, Pilot Vehicle System PVS

Background

Modern aircraft generally take advantage of digital flight control. Flying qualities as well as handling qualities of these control configured vehicles have been specifically tailored to achieve optimal performance for all phases of flight making up the design mission. Thus, original bare airframe dynamics, control law dynamics and finally pilot dynamics are highly interlaced and dependent on each other. Mathematical modelling of the vehicle has matured to a degree that a large portion of the evidences required for certification today can be obtained from validated models rather than flight test. Still, the largest uncertainty remains to be the human pilot. As an adaptive controller he or she is able to introduce a large variety of additional dynamics into the closed loop pilot vehicle system. These sometimes overstress the robustness of the FCS design and can lead to instabilities such as Pilot Involved Oscillations.

Objectives

This AGARDograph is to document existing practices across NATO nations to systematically, effectively and safely test fixed wing aircraft for handling qualities. Methods for identifying deficiencies in the pilot-vehicle-system will be described and experiences in discovering PIO susceptibility will be given. A summary will show how these techniques support the certification process ensuring that the aircraft is free of adverse pilot vehicle interactions prior to EIS. This compilation of existing techniques and experiences is to support development and certification processes of new systems like RPAS.

Topics

The topics will cover the certification process for fixed wing aircraft with regard to in-flight handling qualities evaluations and PIO resistance testing.

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