Non-linear aircraft flight path reconstruction review and new advances
JA Mulder, QP Chu, JK Sridhar, JH Breeman… - Progress in aerospace …, 1999 - Elsevier
Aircraft parameter identification techniques have become accepted as indispensable tools in
the evaluation of prototype-and derivative aircraft in flight. Applications include estimation of …
the evaluation of prototype-and derivative aircraft in flight. Applications include estimation of …
[PDF][PDF] Total least squares estimation of aerodynamic parameter of micro coaxial helicopter from flight data
H Muhammad, HP Thien, T Mulyanto - Int. J. Basic Appl. Sci, 2012 - academia.edu
This paper discusses the estimation of the aerodynamic parameter in the mathematical
model of the micro coaxial helicopter from the flight data. The mathematical model of the …
model of the micro coaxial helicopter from the flight data. The mathematical model of the …
[PDF][PDF] In-Flight Thrust Determination by Load Measurement on the Engine Mounting System
H Muhammad, WK Muhardi, BE Sritjahjono - ICAS 2000 CONGRESS, 2000 - icas.org
In-flight thrust measurement is of much interest as it allows, in principle, to verify the
specified engine and propeller performance as well as to quantify the drag of the aircraft …
specified engine and propeller performance as well as to quantify the drag of the aircraft …
Real-time identification of aircraft physical models for fault tolerant flight control
P Chu, JA Mulder, J Breeman - Fault Tolerant Flight Control: A Benchmark …, 2010 - Springer
Introduction The primary goal of aircraft fault tolerant flight control is to recover or maintain
safe flight when failures have occurred. Aircraft failures can be categorized into subsystem …
safe flight when failures have occurred. Aircraft failures can be categorized into subsystem …
[PDF][PDF] In-flight model identification research aimed at developing a flight simulator model
JH Breeman, H Kannemans, M Laban - System Identification for …, 1998 - apps.dtic.mil
In the last decade NLR and Delft University of Technology have conducted an cooperative
research program using the Swearingen Metro II laboratory aircraft. Topics studied in this …
research program using the Swearingen Metro II laboratory aircraft. Topics studied in this …
[PDF][PDF] J. Prijo Kusumo Aero-Gasdynamics and Vibration Laboratory (LAGG-BPPT) N. Gayus PT Industri Pesawat Terbang Nusantara (IPTN) LGM Custers National …
IEONAS VING - 1996 - icas.org
Interference effects on a wing/flap combination and the propeller installation are especially
important at low speed conditions like the second segment-climb with one-engine …
important at low speed conditions like the second segment-climb with one-engine …