J. H. Breeman

发表

In-flight non-intrusive measurement of wing dynamics and of the aileron and flap deflection and deformation

H. W. Jentink, P. Ružicka, H.P.J. Veerman, 2015 .

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

J. H. Breeman, 1983 .

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

J. H. Breeman, 1983 .

AGARD Flight Test Techniques Series. Volume 3. Identification of Dynamic Systems-Applications to Aircraft. Part 2. Nonlinear Analysis and Manoeuvre Design. (L'Identification des Systemes Dynamiques-Applications aux Aeronefs Titre 2; L'analyse non-lineaire et la Conception de la Manoeuvre)

J. H. Breeman, J A Mulder, J. K. Sridhar, 1994 .

HIGH SPEED RE-PROFILING MEASUREMENTS USING AN INERTIAL NAVIGATION SYSTEM

L B de Wit, J. H. Breeman, Ajl Willekens, 1997 .

Lyapunov-based Fault Tolerant Flight Control Designs for a Modern Fighter Aircraft Model

Jan Albert Mulder, E. R. Van Oort, C. C. de Visser, 2009 .

Determination of Performance and Stability Characteristics from Dynamic Manoeuvres with a Transport Aircraft Using Parameter Identification Techniques

J. H. Breeman, L. J. J. Erkelens, A. M. H. Nieuwpoort, 1984 .

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

J. A. Mulder, J. H. Breeman, J. K. Sridhar, 1996 .

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

J. A. Mulder, J. H. Breeman, J. K. Sridhar, 1995 .

Experience with optimal input design for helicopter parameter identification

J. H. Breeman, C. S. Place, J. K. Sridhar, 1996 .

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

J. A. Mulder, J. H. Breeman, M. Baarspul, 1988 .

System Identification for Integrated Aircraft Development and Flight Testing

Mario Innocenti, Marcello R. Napolitano, R. V. Jategaonkar, 1999 .

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

J. H. Breeman, J. L. Simons, J. Simons, 1978 .

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

J. H. Breeman, J. K. Sridhar, R. Vermerris, 1996 .

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

A.M.H. Nieuwpoort, J. H. Breeman, M. Baarspul, 1987 .

NON-LINEAR AIRCRAFT FLIGHT PATH RECONSTRUCTION REVIEW AND NEW ADVANCES

J. A. Mulder, M. Laban, Qiping Chu, 1999 .