Experience with optimal input design for helicopter parameter identification

Identification of SA-330 PUMA dynamic models from flight test data in frequency domain

Frequency domain identification of multivariable state space models- Analysis procedures and user's guide

MIMO identification techniques and software development in the frequency domain for helicopter and flexible aircraft - Technical results 1994

MIMO identification techniques and software development in the frequency domain for helicopter and flexible aircraft - Progress report 1994

Mathematical model identification for flight simulation, based on flight and taxi tests

Determination of the mathematical model for the new dutch government civil aviation flying school flight simulator

Method for determining the time delay of the pitot-static tubing system of aircraft

Parameter identification results of tests in non-steady symmetric flight with the Hawker Hunter Mk VII

This report presents the parameter identification results derived from data recorded during non-steady symmetric flight test manoeuvres with the Hawker Hunter Mk VII laboratory aircraft. This flight test program was executed in co-operation with the Department of Aerospace Engineering of the Delft University of Technology. The reproducibility of...

Evaluation of a method to extract performance data from dynamic maneuvers for a jet transport aircraft

A very accurate measurement system and a data reduction method have been developed to extract performance data from a single dynamic maneuver, in order to reduce the large amoimt of flight hours required for the determination of these data by means of measurements in steady flight. In order to evaluate the applicability of this method to a modem...